CN104963789A - Working method of Laval nozzle effect stamping oxygen production rocket - Google Patents

Abstract

Disclosed is a working method of a Laval nozzle effect stamping oxygen production rocket. The flame of a Laval nozzle (17) is spouted into a Laval nozzle effect device (composed of the Laval nozzle (17), a vacuum chamber (18) and a diffusion pipe (19)). According to the working principle of the Laval nozzle effect rocket, through American engineers, the Laval nozzle is utilized, positive pressure is built at one end, negative pressure is built at the other end, a table tennis ball is made to reach supersonic velocity to crush table tennis bats (please see the substantive examination reference data), the technology is applied to a rocket propelling system, ultrahigh sound velocity flame airflow is generated, the flight speed of the rocket is higher, all valves (8) are closed when the rocket enters the outer space, and the rocket flies in a traditional liquid hydrogen and liquid hydrogen combustion mode; when work in the outer space is finished, the rocket returns to the atmospheric layer, a small rocket on the head is ignited again, the Laval nozzle effect stamping oxygen production rocket is started to return to the ground, and the Laval nozzle effect stamping oxygen production rocket can be repeatedly used and can fly at zero speed, achieve stamping air suction and oxygen production.

Description

Laval nozzle effect punching press oxygen rocket method of work

Technical field

Laval nozzle effect punching press oxygen rocket method of work belongs to aviation and space technology field.For sky and space plane motor and re-entry space vehicle motor.

Background technique

Although space shuttle is a a progressive step compared with nonrecoverable carrier rocket, still have such as faults frequent, many deficiencies such as somewhat expensive.And sky and space plane is different from space shuttle, its ground installation is simple, and safeguard easy to use, operating cost is low, and on common large airport, just energy horizontal take-off and landing, has the flight frequency of general course line airliner.The external form of this aircraft is similar to large-scale supersonic airliner, has the advantage of aircraft more.When aerial flight, make full use of the oxygen in air.What it can be up to a hundred time in addition reuses, and really achieves the advantage of high-effect and low expense.It is estimated, launch near earth satellite expense with its and only have 1/5 of space shuttle, and launch synchronous satellite expense and only need 1/5., also likely expense is down to 1%, this how to have the huge saving energy of temptation and the good method of money! This makes sky and space plane establish oneself in an unassailable position in the business competition of space on the horizon.

Summary of the invention

Laval nozzle effect punching oxygen rocket can take off in zero-speed, active inspiration and fueling are that something or somebody to fall back on portion mouse 1 drives jet suction means (induction chamber 4, Laval nozzle 5, diffusing tube 6 is jet suction means) complete, when the pressure that the speed of rocket enables the air that head-on need come produce meets punching press suction condition, enter punching press air-breathing working method, when pressure can meet oxygen condition, oxygen can be manufactured awing, closeall valve 8 when entering space, use traditional liquid hydrogen and the flight of liquid oxygen combustion manner, at the complete reentry of space work, head mouse is lighted a fire again, start Laval nozzle effect punching press oxygen rocket and return to ground, Laval nozzle effect punching press oxygen rocket is can the rocket of Reusability, the working principle of Laval nozzle effect rocket utilizes Laval nozzle according to American engineer, malleation is set up in one end, the other end sets up negative pressure, make table tennis reach ultrasound velocity and smash table tennis bat (the Laval nozzle part see examination as to substances reference), this technology is used in rocket propulsion system, make the faster of rocket flight.

The appended drawings show

Fig. 1 is many interior air-breathing duct punching press oxygen rocket figure, as shown in Figure 1, when the pressure that rocket speed produces, when can meet punching press suction condition, head mouse 1 quits work, due at a high speed by atmospheric air punching press to a 4 interior air-breathing duct 2, continue to induction chamber 4, portion of air enters arrow firing chamber 7 through diffusing tube 6 (valve on this pipe is in normally open).Another part air, (these two pipes are designed to spread tubulose through two punching press sucking pipes 16, the Laval nozzle be namely exaggerated, open the valve on these two pipes, as needed in the fueling of mouth of pipe place and igniting place can be arranged) air to be pushed in rocket chamber in 7 by the flame of Laval nozzle 5.Meanwhile at fuel adding point 10, fuel adding point 11 is annotated rocket liquid and solid fuel, rocket fuel and air are entered in diffusing tube mix, light a fire in igniting place 9, air and fuel burn in firing chamber 7 produce flame flow through Laval nozzle 17, spray in diffusing tube 19, Laval nozzle 17 and diffusing tube 19 are provided with gap, therefore vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), (malleation of Laval nozzle 17 comes from firing chamber 7 to make Bearing score nozzle 17 create Laval nozzle effect, negative pressure comes from vacuum chamber 18, therefore when flame from rocket nozzle 20 with hypersonic ejection after, make the faster of rocket flight, when the pressure that the speed of rocket flight produces can meet oxygen condition, open the valve 8 on oxygen generation system, air is through oxygen sucking pipe 13, enter oxygen generating plant 14 oxygen, non-oxidising gas after oxygen and impurity are through non-oxidising gas discharge tube 15 (opening the valve 8 on these two pipes), enter below rocket afterbody jet pipe and discharge.

Fig. 2 is many interior air-breathing ducts, single outer air-breathing duct punching press oxygen rocket figure, as shown in Figure 2, when rocket speed can meet punching press suction condition, head mouse quits work, owing to atmospheric air can be stamped at a high speed 4 interior air-breathing ducts 2 and outer air-breathing duct 3 (induction chamber 4 and by-pass air duct 3 are integrally fused together), enter diffusing tube 6, continuing enters in rocket chamber 7, another part air, (these two pipes can be designed to spread tubulose through two punching press sucking pipes 16, the Laval nozzle be namely exaggerated, also in the fueling of mouth of pipe place and igniting place can be set as required, and the valve 8 opened on these two pipelines), air is pushed in rocket chamber 7, meanwhile at fuel adding point 10, fuel adding point 11 is annotated rocket liquid, solid fuel and catalyzer, rocket fuel and air are mixed in diffusing tube, light a fire in igniting place 9, the flame flow produced that burns in firing chamber 7 sprays in diffusing tube 19 through Laval nozzle 17, Laval nozzle 17 and diffusing tube 19 are provided with gap, therefore vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), (malleation of Laval nozzle 17 comes from firing chamber 7 to make Bearing score nozzle 17 create Laval nozzle effect, negative pressure comes from vacuum chamber 18, therefore when flame from rocket nozzle 20 with hypersonic ejection after, make the faster of rocket flight, , when the stamping pressure that the speed of rocket produces can meet pressure needed for oxygen, open all valves 8 of oxygen generation system, air is through oxygen sucking pipe 13, enter oxygen generating plant 14 oxygen, the horn mouth that non-oxidising gas after oxygen and impurity enter rocket afterbody jet pipe through non-oxidising gas discharge tube 15 (opening the valve on these two pipes) is discharged.

Fig. 3 is single outer air-breathing duct punching press oxygen rocket figure, as shown in Figure 3, when rocket speed can meet punching press suction condition, head mouse 1 quits work, the pressure that high speed makes air produce, atmospheric air is stamped into outer air-breathing duct 3, enter diffusing tube 6, continuing enters in rocket chamber 7, another part air, enter two punching press aspirating air pipes 16 (these two pipes to be designed to spread tubulose, the Laval nozzle be namely exaggerated, can as required in the fueling of mouth of pipe place and arrange igniting place, and the valve 8 opened on these two pipelines), import the afterbody of the typhon mouth of diffusing tube 6, together be pushed in rocket chamber 7 with the material in diffusing tube 6, meanwhile at fuel adding point 10, fuel adding point 11 is annotated rocket liquid, solid fuel and catalyzer, light a fire in igniting place 9, the flame flow produced that burns in firing chamber 7 sprays in diffusing tube 19 through Laval nozzle 17, Laval nozzle 17 and diffusing tube 19 are provided with gap, therefore vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), (malleation of Laval nozzle 17 comes from firing chamber 7 to make Bearing score nozzle 17 create Laval nozzle effect, negative pressure comes from vacuum chamber 18, therefore when flame from rocket nozzle 20 with hypersonic ejection after, make the faster of rocket flight, when the pressure that the speed of rocket produces, when can meet oxygen condition, open all valves 8 of oxygen generation system, air is through oxygen sucking pipe 13, enter oxygen generating plant 14, the horn mouth place that non-oxidising gas after oxygen and impurity enter rocket afterbody jet pipe through non-oxidising gas discharge tube 15 (opening the valve 8 on these two pipes) discharges.

Air-breathing duct punching press oxygen rocket figure in Fig. 4 many branch fork dendroids, as shown in Figure 4, when rocket speed meets punching press suction condition, head mouse 1 quits work, the pressure that high speed makes air produce, by in air-breathing duct 2 in atmospheric air punching press to 5 dendroid, through interior air-breathing duct horn mouth 12, spray in diffusing tube 6, meanwhile at fuel adding point 10, fuel adding point 11 is annotated rocket liquid and solid fuel, enter in rocket chamber 7 and burn, make rocket flight, when the speed of rocket can meet punching press suction condition, head mouse quits work, these two pipes (can be designed to spread tubulose through two punching press aspirating air pipes 16 by another part air, the Laval nozzle be namely exaggerated, also can add rocket fuel at the anterior < diffusing tube toy trumpet mouth mouth of pipe place > of these two pipes and igniting place is set according to needs, and the valve 8 opened on these two pipelines), import in diffusing tube 6, in continuous pushed section rocket chamber 7, light a fire in igniting place 9, the flame flow produced that burns in firing chamber 7 sprays in diffusing tube 19 through Laval nozzle 17, Laval nozzle 17 and diffusing tube 19 are provided with gap, therefore vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), (malleation of Laval nozzle 17 comes from firing chamber 7 to make Bearing score nozzle 17 create Laval nozzle effect, negative pressure comes from vacuum chamber 18, therefore when flame from rocket nozzle 20 with hypersonic ejection after, make the faster of rocket flight, when the pressure that the speed of rocket produces, when can meet oxygen condition, open two valves 8 of oxygen generation system, air is through oxygen sucking pipe 13, enter oxygen generating plant 14 oxygen, non-oxidising gas after oxygen and impurity are through non-oxidising gas discharge tube 15, enter below rocket afterbody jet pipe and discharge.

Fig. 5 is Laval nozzle effect punching press oxygen rocket installation, name of parts is carefully shown.

Embodiment

Punching press oxygen rocket method of work is made up of following equipment and parts, head mouse 1, interior air-breathing duct 2 (or, and outer air-breathing duct 3), induction chamber 4, Laval nozzle 5, diffusing tube 6.Rocket chamber 7, valve 8, igniting place 9, fuel adding point (a) 10, fuel adding point (b) 11, interior air-breathing duct horn mouth 12, oxygen sucking pipe 13, oxygen generating plant 14, non-oxygen discharge tube 15, punching press sucking pipe 16, Laval nozzle 17, vacuum chamber 18, diffusing tube 19, rocket nozzle 20, rocket envelope 21.

As shown in Figure 4: after head mouse 1 is lighted a fire, produce high temperature, the flame gas of high pressure, spray from the flame of Laval nozzle 5 (nozzle group) with funnel-like, meet at a bit, funnel-like flame kernel can produce vacuum (principle is similar to flow eddies), air air-breathing duct 2 in dendroid is sucked in induction chamber 4, and high velocity jet is in diffusing tube 6, the flame of Laval nozzle 5 (nozzle group) meets at a bit with funnel-like, distance (being that vacuum produces important indicator) is set between flame intersection point and diffusing tube 6, air and fuel are sucked drawn and to spray into nozzle that diffusing tube 6 is continuous to be entered in rocket chamber 7, meanwhile fuel adding point 10, fuel adding point 11 is annotated rocket liquid, solid fuel and urge agent, mix at diffusing tube 6, light in igniting place 9, burn in firing chamber 7 produce flame flow through Laval nozzle 17, spray in diffusing tube 19, Laval nozzle 17 and diffusing tube 19 are provided with gap, therefore vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), (malleation of Laval nozzle 17 comes from firing chamber 7 to make Bearing score nozzle 17 create Laval nozzle effect, negative pressure comes from vacuum chamber 18, therefore when flame from rocket nozzle 20 with hypersonic ejection after, make the faster of rocket flight, when flying speed can meet punching press suction condition, head mouse quits work, portion of air and fuel, enter in diffusing tube 6 through induction chamber 4, at fuel adding point 10, the fueling of fuel adding point 11, enter rocket chamber 7, another part air (opens the valve 8 in this system through two punching press sucking pipes 16, punching press sucking pipe can be designed to Laval nozzle shape, if need also at these two mouth of pipe place filling rocket fuels and igniting place to be arranged) import diffusing tube 6 and the material in diffusing tube 6, after igniting place 9 is lighted a fire, burn in fuel chambers 7, make rocket flight, when the stamping pressure that rocket speed produces can meet Oxygen Condition processed, another part air, through oxygen sucking pipe 13 (opening the valve 8 on these two pipes), air is pressed into oxygen generating plant 14 oxygen, non-oxidising gas after oxygen and impurity, enter below rocket afterbody jet pipe through non-oxygen discharge tube 15 (opening the valve 8 on these two pipes) and discharge.

Close all valves 8 after entering space, make firing chamber 7 can meet space flight needs.

The closeall valve 8 when entering space, traditional liquid hydrogen and liquid oxygen combustion manner is used to fly, at the complete reentry of space work, head mouse is lighted a fire again, start Laval nozzle effect punching press oxygen rocket and return to ground, Laval nozzle effect punching press oxygen rocket is can repeatedly with the rocket made.

Claims (10)

1. punching press oxygen rocket method of work is made up of following equipment and parts, head mouse 1, interior air-breathing duct 2 (or, with outer air-breathing duct 3), induction chamber 4, Laval nozzle 5, diffusing tube 6, rocket chamber 7, valve 8, igniting place 9, fuel adding point 10, fuel adding point 11, interior suction duct horn mouth 12, oxygen sucking pipe 13, oxygen generating plant 14, non-oxygen discharge tube 15, punching press sucking pipe 16, Laval nozzle 17, vacuum chamber 18, diffusing tube 19, rocket nozzle 20, rocket envelope 21, the Laval nozzle effect punching press oxygen rocket be made up of 1-21 equipment and parts can take off in zero-speed, can punching press air-breathing, oxygen in-flight, the oxygen of preparation can be used in space, complete the work of space, head mouse can be rekindled, restart rocket flight backspace ground freely, this rocket is can the rocket of Reusability.

2. utilize the pressure of punching press to carry out oxygen, the valve 8 that interior air-breathing duct bell-mouthed design 2/ oxygen sucking pipe 16 is arranged, valve 8 on valve 8/ diffusing tube 6 that the valve 8/ oxygen sucking pipe 13 that non-gas discharge tube 15 is arranged is arranged designs/setting/interior air-breathing duct horn mouth 12 of filling point 10 and fuel adding point 11 position, telescopic Laval nozzle shape can be designed to, tubulose/punching press sucking pipe 16 can also be designed to and can be designed to tubulose, Laval nozzle shape, also tubulose can be designed to, fuel adding point and igniting place/oxygen sucking pipe 13 can be designed to tubulose can also be set in this pipe front end, Laval nozzle shape, bell mouth shape.

3. sparger (examination as to substances reference sparger part please be read) vacuum work principle, enable rocket suck air/Laval nozzle means for influencing (Laval nozzle 17 in atmospheric layer, vacuum chamber 18, diffusing tube 19) the suction tude of design/punching press sucking pipe 16, being connected to air-breathing in dendroid contains on the branch fork of 2, the air inlet of oxygen sucking pipe 13, be connected to air-breathing in dendroid contain 2 branch fork upper/when rocket speed enables the pressure of punching press meet punching press suction condition, head mouse 1 quits work, enter punching press aspirated mode/rocket in aerial flight, to manufacture oxygen/air-breathing rocket atmospheric layer that flies out enter space, throttle down 8 makes rocket chamber 7 can meet space flight requirement 7.

Within 4. Dogan inspiratory bypass -- -- -- -- -- -- -- 1 head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point 10 to fuel, fuel injection points11-------1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- a ram air suction pipe16------1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- multiple points to 10 points to fuel, fuel filling 11 -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition point 9 -- -- -- -- -- - 1 oxygen inhalation tube13-----114 a oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge tube15------A rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube more than 13 -- -- -- -- -- oxygen generating equipment14-------1A non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber7------- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle17-----1A vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- 1 head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13-1 psa equipment14-------1A non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13-1 psa equipment14-------A non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition point 9 -- -- -- -- -- - 1 oxygen inhalation tube13-----14 one oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel filling point 11 -- -- -- -- -- -- -- multiple stamping the suction 16 -- -- -- -- -- - 1 ignition point 9 -- -- -- -- -- - 1 oxygen inhalation tube13-----14 one oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- more pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel filling point 11 -- -- -- -- -- -- -- multiple stamping the suction 16 -- -- -- -- -- - multiple ignition point 9 -- -- -- -- -- - more oxygen inhalation tube13-----14 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- more pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge tube15------1A rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber and a diffusion tube -- -- -- -- -- - 1 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more than the head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge tube15------Multiple rocket combustion chamber 7 -- -- -- -- -- -- -- more than 17 -- -- -- -- -- a laval nozzle vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group) -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / single suction bypass (with laval nozzle group)-------More head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20.

5. Single suction duct outside -- -- -- -- -- -- -- 1 head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube19-------1Rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction duct-------More head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction duct-------More head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle5------Multiple diffusion tube 6 -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- (1) the oxygen outlet pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber and a diffusion tube -- -- -- -- -- - 1 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- more pressing suction tube16------Multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition point 9 -- -- -- -- -- - more oxygen inhalation tube13-----14 more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge tube15------Multiple rocket combustion chamber 7 -- -- -- -- -- -- -- more than 17 -- -- -- -- -- a laval nozzle vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- 1 head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition point 9 -- -- -- -- -- - 1 oxygen inhalation tube13-----14 one oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition point 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment are -- -- -- -- -- -- -- a non oxygen discharge tube15------A rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injectors, 11 -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber18------A diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20 / single suction duct-------More head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle5------Multiple diffusion tube 6 -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- (1) the oxygen outlet pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection points11-------Multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber18------Multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / suction duct outside -- -- -- -- -- -- -- more than the head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20.

6. Multiple root inside inspiratory bypass with multiple root inspiratory outside bypass -- -- -- -- -- -- -- 1 head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle17-----A vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more than the head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19-------Inhale within one rocket nozzle of more than 20 / bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injectors, 11 -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17-----A vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more than the head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13-1 psa equipment 14-------A non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- multiple points to 10 points to fuel, fuel filling more than 11 -- -- -- -- -- -- -- stamping the suction 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - multiple diffusion tube 6 -- -- -- -- -- -- -- more than 10, fuel filling points to fuel 11 -- -- -- -- -- -- -- more pressing suction tube 16------Multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan breathe in bypass-------More head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injectors, 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19-------Inhale within one rocket nozzle of more than 20 / bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13-14 more oxygen generation equipment are -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and dogan inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injectors, 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber18------Multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- 1 head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13-1 psa equipment 14------- 1 the oxygen outlet pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7-------A laval nozzle 17 -- -- -- -- -- a vacuum chamber and a diffusion tube -- -- -- -- -- - 1 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more than the head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7------- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge tube 15------A rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition point 9 -- -- -- -- -- - more oxygen inhalation tube 13-----14 more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- multiple points to fuel 10, 11 points to fuel -- -- -- -- -- -- - multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- (1) the oxygen outlet pipe 15 -- -- -- -- -- - multiple rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber and a diffusion tube -- -- -- -- -- - 1 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5------Multiple diffusion tube 6 -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- (1) the oxygen outlet pipe 15 -- -- -- -- -- - multiple rocket combustion chamber 7 -- -- -- -- -- -- -- more than 17 -- -- -- -- -- a laval nozzle vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- 1 head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- - a stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 -- -- -- -- -- a laval nozzle 5------A diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- - a stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5------Multiple diffusion tube 6 -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- (1) the oxygen outlet pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber and a diffusion tube -- -- -- -- -- - 1 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection points 11-------Multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection points 11-------Multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- more room to breathe in 4-----Multiple laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition point 9 -- -- -- -- -- - more oxygen inhalation tube 13-----14 more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20.

7. Two branches fork dendritic inspiratory bypass -- -- -- -- -- -- -- 1 head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber18------A diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle17-----A vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge tube15------A rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside inspiratory bypass and single suction bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- multiple points to fuel 10、Tanking point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- more pressing suction tube16------Multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5------Multiple diffusion tube 6 -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- (1) the oxygen outlet pipe 15 -- -- -- -- -- - multiple rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube19-------1A rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injectors, 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20.

More than 8 branch fork dendritic inspiratory bypass -- -- -- -- -- -- -- 1 head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- a suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube19-------A rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 -- -- -- -- -- a laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 -- -- -- -- -- - a diffusion tube 6 -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / dendritic branch fork breathe in bypass-------More head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- 1 point to fuel 10, 11 points to fuel -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- 1 stamping the suction 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / dendritic branch fork breathe in bypass-------More head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - 1 ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - 1 oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle within 20 / dendritic branch fork breathe in bypass-------More head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injectors, 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber18------A diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- -- a rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge tube15------Multiple rocket combustion chamber 7 -- -- -- -- -- -- -- a laval nozzle 17 -- -- -- -- -- a vacuum chamber and a diffusion tube -- -- -- -- -- - 1 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - a diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- more room to breathe in4-----Multiple laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- (1) the oxygen outlet pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / dendritic branches fork inside inspiratory bypass -- -- -- -- -- -- -- more head small rocket 1 -- -- -- -- -- -- -- multiple suction chamber 4 - laval nozzle 5 multiple diffusion tube 6 -- -- -- -- -- - -- -- -- -- -- -- -- more than 10 points to fuel, fuel injection point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place more than 9 -- -- -- -- -- - oxygen inhalation tube 13 14 -- -- -- -- -- more oxygen generation equipment -- -- -- -- -- -- -- a non oxygen discharge pipe 15 -- -- -- -- -- - multiple rocket combustion chamber more than 7 -- -- -- -- -- -- - laval nozzle 17 -- -- -- -- -- a vacuum chamber 18 -- -- -- -- -- - multiple diffusion tube 19 -- -- -- -- -- -- -- a rocket nozzle 20.

9. the flame of Laval nozzle 17 sprays into Laval nozzle means for influencing (Laval nozzle 17, vacuum chamber 18, diffusing tube 19, your means for influencing of Bearing score nozzle indication be exactly these 3 parts), the working principle of Laval nozzle effect rocket utilizes Laval nozzle according to American engineer, malleation is set up in one end, the other end sets up negative pressure, make table tennis reach ultrasound velocity and smash table tennis bat (the Laval nozzle part see examination as to substances reference), this technology is used in rocket propulsion system, produce hypersonic flame flow, make the speed of rocket flight faster.

10. the method for work of your effect Bearing score nozzle effect punching press oxygen rocket, relate to and belong to aviation and space technology field, there are 2 punching press air-breathing and oxygen separating functions, can take off in zero-speed, active inspiration and fueling be that something or somebody to fall back on portion mouse (needing traditional rocket of liquid oxygen work) drives jet suction means to complete, closeall valve 8 when entering space, traditional liquid hydrogen and liquid oxygen combustion manner is used to fly, at the complete reentry of space work, head mouse is lighted a fire again, starts Laval nozzle effect punching press oxygen arrow and returns to ground.