CN105065138A

CN105065138A - Working method of detonation punching oxygen-generation rocket based on Laval nozzle effect

Info

Publication number: CN105065138A
Application number: CN201510427121.9A
Authority: CN
Inventors: 杜善骥
Original assignee: Individual
Current assignee: Individual
Priority date: 2015-07-19
Filing date: 2015-07-19
Publication date: 2015-11-18

Abstract

Rocket propellants used by a detonation punching oxygen-generation rocket based on the Laval nozzle effect are explosives, and thus a higher propelling speed can be obtained; on the basis, the Laval nozzle effect (please refer to the Laval nozzle part in substantive examination reference data) technique is applied to a rocket propelling system so that the speed of a rocket can be higher, in this way, the air punching pressure can meet the oxygen generation condition and meet the requirement for oxygen production, and both an active air suction function and a passive punching air suction function are achieved. The rocket can take off at the zero speed; all valves 8 are closed when the rocket enters the outer space, and the rocket flies in a traditional liquid hydrogen and liquid oxygen combustion way and returns to the atmosphere after work in the outer space is finished; a small rocket on the head is ignited again to drive a jet flow air suction device to suck air actively, and the detonation punching oxygen-generation rocket based on the Laval nozzle effect is started to return to the ground. The detonation punching oxygen-generation rocket based on the Laval nozzle effect can be used repeatedly.

Description

Laval nozzle effect detonation punching press oxygen rocket method of work

Technical field

Laval nozzle effect detonation 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 detonation punching oxygen rocket can take off in zero-speed, active inspiration and fuel (explosive) filling and mixing be something or somebody to fall back on portion mouse 1 (being need the traditional rocket with liquid oxygen work) drive jet suction means (interior air-breathing duct 2 < or, with outer air-breathing duct 3 > induction chamber 4, Laval nozzle 5, diffusing tube 6 is jet suction means) (the sparger part in examination as to substances reference please be read) that complete, when the pressure that the speed of rocket enables the air that head-on need come produce meets punching press suction condition, head mouse quits work, enter punching press air-breathing working method, when pressure can meet oxygen liquefaction oxygen condition, oxygen can be manufactured, closeall valve 8 when entering space, use traditional liquid hydrogen and the flight of liquid oxygen working method, at the complete reentry of space work, head mouse is lighted a fire again, start Laval nozzle effect detonation punching press oxygen rocket and return to ground, Laval nozzle effect detonation punching press oxygen rocket is can the rocket of Reusability, because the rocket propellant used is explosive, therefore larger speed can be obtained, the working principle of Laval nozzle effect detonation punching press oxygen 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 applied in rocket propulsion system, make the faster of rocket flight.

The appended drawings show

Fig. 1 is many interior air-breathing duct detonation 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, at fuel adding point 10, fuel adding point 11 is annotated rocket liquid and solid fuel (explosive), air mixes in diffusing tube 6 (valve 8 on this pipe is in normally open) with rocket fuel (explosive), these two pipes (can be designed to Laval nozzle through two punching press sucking pipes 16 by another part air, open the valve 8 on these two pipes, at air intlet place filling rocket fuel < explosive > and igniting place can be set as needs), import diffusing tube 6 typhon mouth place, light a fire in igniting place 9, detonation is produced in firing chamber 7, detonation wave is through Laval nozzle 17, spray in diffusing tube 19, vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), Bearing score nozzle 17 can produce Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of Laval nozzle 17 comes from firing chamber 7, negative pressure comes from vacuum chamber 18, therefore when detonation wave sprays from rocket nozzle 20, make the faster of rocket flight, when the pressure that the speed of rocket flight enables air produce meets oxygen condition, open all valves 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, enter below rocket afterbody jet pipe and discharge.

Fig. 2 is many interior air-breathing ducts, single outer air-breathing duct detonation punching press oxygen rocket figure, as shown in Figure 2, when rocket speed can meet punching press suction condition, head mouse 1 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), at fuel adding point 10, fuel adding point 11 is annotated rocket liquid and solid fuel (explosive), air mixes in diffusing tube 6 (valve 8 on this pipe is in normally open) with rocket fuel (explosive), these two pipe Front-end Design (can be become Laval nozzle shape through two punching press sucking pipes 16 by another part air, open the valve 8 on these two pipes, at air intlet place filling rocket fuel < explosive > and igniting place can be set as needs), import diffusing tube 6 typhon mouth place, light a fire in igniting place 9, detonation is produced in firing chamber 7, detonation wave is through Laval nozzle 17, spray in diffusing tube 19, vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), Bearing score nozzle 17 can produce Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of Laval nozzle 17 comes from firing chamber 7, negative pressure comes from vacuum chamber 18, therefore when detonation wave sprays from rocket nozzle 20, make the faster of rocket flight, when the pressure that the speed of rocket flight enables air produce meets oxygen condition, open all valves 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, enter below rocket afterbody jet pipe and discharge.

Fig. 3 is single outer air-breathing duct detonation punching press oxygen rocket figure, as shown in Figure 3, when rocket speed can meet punching press suction condition, head mouse 1 quits work, because high speed makes air punching press to outer air-breathing duct 3, at fuel adding point 10, fuel adding point 11 is annotated rocket liquid and solid fuel (explosive), air mixes in diffusing tube 6 (valve 8 on this pipe is in normally open) with rocket fuel (explosive), these two pipes (can be designed to Laval nozzle through two punching press sucking pipes 16 by another part air, open the valve 8 on these two pipes, at air intlet place filling rocket fuel < explosive > and igniting place can be set as needs), import diffusing tube typhon mouth, light a fire in igniting place 9, detonation is produced in firing chamber 7, detonation wave is through Laval nozzle 17, spray in diffusing tube 19, vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), Bearing score nozzle 17 can produce Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of Laval nozzle 17 comes from firing chamber 7, negative pressure comes from vacuum chamber 18, therefore when detonation wave sprays from rocket nozzle 20, make the faster of rocket flight, when the pressure that the speed of rocket flight produces can meet oxygen condition, open all valves 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, enter below rocket afterbody jet pipe and discharge.

Air-breathing duct detonation 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, high speed to make in air punching press to 5 dendroid in air-breathing duct 2, through Laval nozzle 12, at fuel adding point 10, fuel adding point 11 is annotated rocket liquid and solid fuel (explosive), air mixes in diffusing tube 6 (valve 8 on this pipe is in normally open) with rocket fuel (explosive), these two pipes (can be designed to Laval nozzle through two punching press sucking pipes 16 by another part air, open the valve 8 on these two pipes, at air intlet place filling rocket fuel < explosive > and igniting place can be set as needs), import diffusing tube typhon mouth, light a fire in igniting place 9, detonation is produced in firing chamber 7, detonation wave is through Laval nozzle 17, spray in diffusing tube 19, vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), Bearing score nozzle 17 can produce Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of Laval nozzle 17 comes from firing chamber 7, negative pressure comes from vacuum chamber 18, therefore when detonation wave sprays from rocket nozzle 20, make the faster of rocket flight, when the pressure that the speed of rocket flight produces can meet oxygen condition, open all valves 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, enter below rocket afterbody jet pipe and discharge.

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

Embodiment

Laval nozzle effect blast 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 10, fuel adding point 11, Laval nozzle 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), by air air-breathing duct 2 in dendroid, Laval nozzle 12 sucks through induction chamber 4, fuel adding point 10, fuel adding point 11 is annotated rocket liquid, solid fuel (explosive) and urge agent, pushed by the flame flow of Laval nozzle 5 (nozzle group) and mix at diffusing tube 6, induction chamber 4 can produce and can produce vacuum (please read the sparger part in examination as to substances reference), the inlet capacity of air and rocket fuel (explosive) can be strengthened, light in igniting place 9, the detonation wave of pinking generation is produced through Laval nozzle 17 in firing chamber 7, spray in diffusing tube 19, vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), Bearing score nozzle 17 creates Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of Laval nozzle 17 comes from firing chamber 7, negative pressure comes from vacuum chamber 18, therefore when detonation wave sprays from rocket nozzle 20, make the faster of rocket flight.When rocket speed meets punching press suction condition, head mouse 1 quits work, high speed to make in air punching press to 5 dendroid in air-breathing duct 2, through Laval nozzle 12, at fuel adding point 10, fuel adding point 11 is annotated rocket liquid and solid fuel (explosive), air mixes in diffusing tube 6 (valve 8 on this pipe is in normally open) with rocket fuel (explosive), these two pipes (can be designed to Laval nozzle through two punching press sucking pipes 16 by another part air, open the valve 8 on these two pipes, at air intlet place filling rocket fuel < explosive > and igniting place can be set as needs), import diffusing tube typhon mouth, light a fire in igniting place 9, detonation is produced in firing chamber 7, detonation wave is through Laval nozzle 17, spray in diffusing tube 19, vacuum chamber 18 can produce vacuum (please read the sparger part of examination as to substances reference), Bearing score nozzle 17 can produce Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of Laval nozzle 17 comes from firing chamber 7, negative pressure comes from vacuum chamber 18, therefore when detonation wave sprays from rocket nozzle 20, make the faster of rocket flight, when the pressure that the speed of rocket flight produces can meet oxygen condition, open all valves 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, enter below rocket afterbody jet pipe and discharge.

Close all valves 8 after entering space, use liquid hydrogen and liquid oxygen flying method.

The rocket propellant that Laval nozzle effect detonation punching press oxygen rocket uses is explosive, therefore can obtain and larger push away speed, on this basis Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference) technology is used in rocket propulsion system, rocket can be made to produce higher speed, therefore enable the pressure of air punching press meet oxygen condition and oxygen manufacture, and have active inspiration and passive punching press air suction function.This rocket can zero-speed take off, when entering space, closeall valve 8 uses 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 and is driven jet suction means active inspiration, start Laval nozzle effect pinking ram rocket and return to ground, Laval nozzle effect detonation ram rocket is can repeatedly with the rocket made.

Claims

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, 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 10, fuel adding point 11, Laval nozzle 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.

2. utilize the pressure of punching press to carry out oxygen, the valve 8 that the position setting/oxygen sucking pipe 16 of Laval nozzle 12 is arranged, the valve 8 that the design/oxygen sucking pipe 13 of the valve 8 that non-gas discharge tube 15 is arranged is arranged uses/diffusing tube 6 on valve 8 design/setting/Laval nozzle 12 of filling point 10 and fuel adding point 11 position can be designed to telescopic Laval nozzle, Laval nozzle 12 is designed to tubulose/punching press sucking pipe 16 can be designed to tubulose, Laval nozzle shape, fuel adding point and igniting place/oxygen sucking pipe 13 can be designed to tubulose are set at air intlet place.

3. sparger (examination as to substances reference sparger part please be read) vacuum work principle, be used in rocket active inspiration/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 air punching press meet punching press suction condition, head mouse 1 quits work, enter passive 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 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 than small rocket 1 head-------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 -- -- -- -- -- -- -- 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 inspiratory bypass in more than 20 / root-------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 -- -- -- -- -- - -- -- -- -- -- -- -- 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 -- -- -- -- -- -- -- 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 injectors, 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 -- -- -- -- -- -- -- 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 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 chamber 18 -- -- -- -- -- - a diffusion tube 19-------Inhale within one rocket nozzle of more than 20 / 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 -- -- -- -- -- - 7 multiple rocket combustion chamber-------A laval nozzle 17 -- -- -- -- -- a vacuum chamber and a diffusion tube -- -- -- -- -- - 1 19 -- -- -- -- -- -- -- a rocket nozzle of more than 20 / inside 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 -- -- -- -- -- - 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 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-------Inhale within one rocket nozzle of more than 20 / 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 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 -- -- -- -- -- -- -- 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 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 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 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 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 / 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 -- -- -- -- -- - 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 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 -- -- -- -- -- - 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 charging point 11 -- -- -- -- -- -- -- multiple pressing suction pipe 16 -- -- -- -- -- - multiple ignition place 9 -- -- -- -- -- - more oxygen inhalation tube 13 14 -- -- -- -- -- 1 oxygen generation equipment are studied-------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 -- -- -- -- -- - -- -- -- -- -- -- -- 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 -- -- -- -- -- 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 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 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 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 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 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 -- -- -- -- -- -- -- more 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 tube 19------- a rocket nozzle 20 / single suction bypass------- more than small rocket 1 head-------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 bypass------- more head small rocket more than 1------- breathe in room 4-----Multiple 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-------Outside a rocket nozzle 20 / single suction 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------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 injectors, 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-------Outside a rocket nozzle 20 / single suction 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 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 more than 1------- breathe in room 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------- (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 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 than small rocket 1 head-------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 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 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------7 multiple rocket combustion chamber-------Multiple 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 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 / 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 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----- 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 are studied-------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 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----- -------- 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 are studied-------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------- 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 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 bypass------- more head small rocket 1------- multiple suction chamber 4-laval nozzle 5 multiple diffusion tube 6-------------- more than 10 points to arg, arg, 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 than small rocket 1 head-------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------ 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 than small rocket 1 head-------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 / 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 are studied-------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 / 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 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 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----- 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 and a diffusion tube------1 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----- -------- 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 charging point 11------- 1 stamping the suction 16------1 ignition place 9------1 oxygen inhalation tube 13-14 (1) oxygen generation equipment are studied-------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------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-------Multiple points to 10 points to fuel, fuel filling more than 11------- stamping the suction 16------multiple 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 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----- 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 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------ 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------- 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 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------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 charging point 11------- multiple pressing suction pipe 16------multiple ignition point 9------Multiple 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 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------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 filling point 11------- more 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------- 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-------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----- a laval nozzle 5------a diffusion tube 6------- 1 point 10 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------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------- 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 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------- more 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 10 points to fuel, fuel filling 11------- multiple pressing suction pipe 16------multiple ignition point 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 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------- (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-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 than small rocket 1 head-------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------ 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------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------- 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 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 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 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----- -------- 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------- 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 than the 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 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------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------- 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----- -------- 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 injectors, 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 17-18 a vacuum chamber------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 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 9------more 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----- -------- 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 charging point 11------- multiple pressing suction pipe 16------multiple ignition place 9------more oxygen inhalation tube 13 14----- more oxygen generation equipment are studied-------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 filling 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------- 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 are studied-------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------- 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 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----- 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 chamber and a diffusion tube------1 19------- a rocket nozzle within 20 / two branch fork dendritic 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 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 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----- -------- 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 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------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------- multiple pressing suction pipe 16------multiple ignition place 9------1 oxygen inhalation tube 13-14 (1) oxygen generation equipment are studied-------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 filling 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------- multiple pressing suction pipe 16------multiple ignition point 9------Multiple 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------- 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 9------more oxygen inhalation tube 13 14----- more oxygen generation equipment are studied-------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 / 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 tube 19------- a rocket nozzle within 20 / two branch fork dendritic inspiratory bypass------- more than small rocket 1 head-------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 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.

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 and a diffusion tube ------ 1 19 -------a rocket nozzle of more than 20 / dendritic branches fork inside 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 / 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 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 ------ -------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 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 ------ 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 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 -----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 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 ------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 / dendritic branches fork inside 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 ------ 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 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 / 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 more than 1 -------breathe in room 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 -------(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 rocket propellant that Laval nozzle effect detonation punching press oxygen rocket uses is explosive, therefore can obtain and larger push away speed, on this basis Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference) technology is used in rocket propulsion system, rocket can be made to produce higher speed, therefore enable the pressure of air punching press meet oxygen condition and oxygen manufacture, and have active inspiration and passive punching press air suction function.This rocket can zero-speed take off, when entering space, closeall valve 8 uses 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 and is driven jet suction means active inspiration, start Laval nozzle effect pinking ram rocket and return to ground, Laval nozzle effect detonation ram rocket is can repeatedly with the rocket made.