CN105134411A

CN105134411A - Working method of detonation ram Laval nozzle effect propelled and oxygen-producing rocket

Info

Publication number: CN105134411A
Application number: CN201510557721.7A
Authority: CN
Inventors: 杜善骥
Original assignee: Individual
Current assignee: Individual
Priority date: 2015-09-02
Filing date: 2015-09-02
Publication date: 2015-12-09

Abstract

A detonation ram Laval nozzle effect propelled and oxygen-producing rocket uses explosive as a rocket propellant, so that higher propulsion speed and larger propulsion power are obtained. On the basis, the technology of the Laval nozzle effect (described in the Laval nozzle effect section of substantial examination reference materials) is adopted in a rocket propulsion system to enable the speed of the rocket to be higher, and the rocket can produce oxygen in flight when the ram pressure of air can meet the oxygen-producing conditions. The rocket can take off at zero speed, all valves 8 are turned off and the rocket flies in a traditional liquid hydrogen and liquid oxygen combustion mode when the rocket goes into the space. After space work is completed, the rocket returns to an atmospheric layer, a small rocket at the head portion is ignited again, and a jet flow air-suction device is driven to initiatively suck air so as to enable the detonation ram Laval nozzle effect propelled and oxygen-producing rocket to return to the ground. The detonation ram Laval nozzle effect propelled and oxygen-producing rocket can be repeatedly used.

Description

Detonation punching press Laval nozzle effect advances and oxygen rocket method of work

Technical field

Detonation punching press Laval nozzle effect advances and 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

Detonation punching press Laval nozzle effect advances and oxygen rocket can take off in zero-speed, active inspiration and fuel (explosive) filling and mix with air 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 oncoming air 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, Laval nozzle effect state can be entered and manufacture oxygen, 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, startup detonation punching press Laval nozzle effect advances and oxygen rocket returns to ground, detonation punching press Laval nozzle effect advances and oxygen rocket is can the rocket of Reusability, because the rocket propellant used is explosive, therefore larger speed can be obtained, detonation punching press Laval nozzle effect advances and oxygen rocket working principle 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 and oxygen generation system, make the propelling of rocket flight and oxygen more powerful.

The appended drawings show

Fig. 1 is that many interior air-breathing duct detonation punching press Laval nozzle effects advance and 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 by induction chamber 4 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 required), import diffusing tube 6 typhon mouth place, light a fire in igniting place 9, import in firing chamber 7 and produce detonation, 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 the detonation wave creating Laval nozzle effect 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 (the air intlet place of this pipe is designed to Laval nozzle), enter oxygen generating plant 14 oxygen, non-oxidising gas after oxygen and impurity are through non-oxidising gas discharge tube 15, access vacuum chamber 18, through diffusing tube 19, continue and discharge through rocket nozzle 20, the malleation of oxygen sucking pipe 13 (Laval nozzle), derive from ram-air, its negative pressure comes from vacuum chamber 18, now oxygen sucking pipe 13 (this pipe air intlet place is designed to Laval nozzle) can produce Lavalle effect, therefore air anxious high speed can bang into oxygen generating plant oxygen.

Fig. 2 is many interior air-breathing ducts, single outer air-breathing duct detonation punching press Laval nozzle effect advances and 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), this Liang Genguan front end air inlet (can be designed to Laval nozzle by air-breathing duct 3 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, import in firing chamber 7 and produce detonation, 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 (the air intlet place of this pipe is designed to Laval nozzle), enter oxygen generating plant 14 oxygen, non-oxidising gas after oxygen and impurity are through non-oxidising gas discharge tube 15, access vacuum chamber 18, through diffusing tube 19, continue and discharge through rocket nozzle 20, the malleation of oxygen sucking pipe 13 (Laval nozzle), derive from ram-air, its negative pressure comes from vacuum chamber 18, now oxygen sucking pipe 13 (this pipe air intlet place is designed to Laval nozzle) can produce Lavalle effect, therefore air anxious high speed can bang into oxygen generating plant oxygen.

Fig. 3 is that single outer air-breathing duct detonation punching press Laval nozzle effect advances and 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 pipe air intlets (can be designed to Laval nozzle by air-breathing duct 3 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 enables air produce meets oxygen condition, open the valve 8 on oxygen sucking pipe 13 (this pipe is designed to Laval nozzle shape), air bangs into the non-oxidising gas after oxygen generating plant 14 oxygen, oxygen through oxygen sucking pipe 13 and impurity accesses vacuum chamber 18 through non-oxygen discharge tube 15 (opening the valve 8 on this pipe), through diffusing tube 19, continues and discharge through rocket nozzle 20.Lavalle effect oxygen principle is such: the malleation of oxygen sucking pipe 13 (Laval nozzle), derive from ram-air, its negative pressure comes from vacuum chamber 18, now oxygen sucking pipe 13 (this pipe air intlet place is designed to Laval nozzle) can produce Lavalle effect, and therefore air can bang into oxygen generating plant oxygen with anxious high speed.

Fig. 4 is that in many branch fork dendroids, air-breathing duct detonation punching press Laval nozzle effect advances and oxygen rocket figure, as shown in Figure 4, when rocket speed meets punching press suction condition, head mouse 1 quits work, air to be stamped to 5 dendroids 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 by two, another portion punching press sucking pipe 16, 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 enables air produce meets oxygen condition, open all valves 8 on oxygen generation system, air is through oxygen sucking pipe 13 (the air intlet place of this pipe is designed to Laval nozzle), enter oxygen generating plant 14 oxygen, non-oxidising gas after oxygen and impurity are through non-oxidising gas discharge tube 15, access vacuum chamber 18, through diffusing tube 19, continuous through rocket nozzle 20 discharge, the malleation of oxygen sucking pipe 13 (Laval nozzle), derive from ram-air, its negative pressure comes from vacuum chamber 18, now oxygen sucking pipe 13 (this pipe air intlet place is designed to Laval nozzle) can produce Lavalle effect, therefore air anxious high speed can bang into oxygen generating plant oxygen.

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

Embodiment

Detonation punching press Laval nozzle effect advances and oxygen rocket method of work forming by 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 diffusing tube 6 by the flame flow of Laval nozzle 5 (nozzle group) to mix, induction chamber 4 can produce vacuum (please read the sparger part in examination as to substances reference), the suction of air and the injection intensity of Laval nozzle flame 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, the high speed of rocket 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 enables air produce meets oxygen condition, open all valves 8 on oxygen generation system, air is through oxygen sucking pipe 13 (the air intlet place of this pipe is designed to Laval nozzle), enter oxygen generating plant 14 oxygen, non-oxidising gas after oxygen and impurity are through non-oxidising gas discharge tube 15, access vacuum chamber 18, through diffusing tube 19, continue and discharge through rocket nozzle 20, the malleation of oxygen sucking pipe 13 (Laval nozzle), derive from ram-air, its negative pressure comes from vacuum chamber 18, now oxygen sucking pipe 13 (this pipe air intlet place is designed to Laval nozzle) can produce Lavalle effect, therefore air anxious high speed can bang into oxygen generating plant oxygen.

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

The rocket propellant that detonation punching press Laval nozzle effect advances and oxygen rocket uses is explosive, therefore can obtain and larger push away speed and thrust, 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, when the pressure of air punching press can meet oxygen condition, rocket can manufacture oxygen awing.This rocket can zero-speed take off, closeall valve 8 when entering space, traditional liquid hydrogen and liquid oxygen combustion manner is used to fly, at the complete reentry of space work, head mouse is lighted a fire again and is driven jet suction means active inspiration, make the propelling of detonation punching press Laval nozzle effect and oxygen rocket return to ground, Laval nozzle effect detonation ram rocket is can repeatedly with the rocket made.

Claims

1. the propelling of detonation punching press Laval nozzle effect and oxygen rocket are made up of following equipment and parts, head mouse 1, interior air-breathing duct 2 (or, with outer air-breathing duct 3), induction chamber 4, Laval nozzle 5 (or Laval nozzle 5 < nozzle group >), 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. the valve 8 on valve 8/ diffusing tube 6 that the valve 8/ oxygen sucking pipe 13 that the valve 8/ non-gas discharge tube 15 that rocket utilizes the pressure of punching press to arrange on the position setting/oxygen sucking pipe 16 manufacturing oxygen/Laval nozzle 12 is awing arranged is arranged designs/and the setting/Laval nozzle 12 of filling point 10 and fuel adding point 11 position can be designed to telescopic Laval nozzle/punching press sucking pipe 16 and can be designed to tubulose, Laval nozzle shape, arrange at air intlet place fuel adding point and igniting place/.

3. head mouse 1 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 called jet suction means) produce vacuum (the sparger part of examination as to substances reference please be read), for air-breathing rocket sucks air/Laval nozzle means for influencing (Laval nozzle 17 in atmospheric layer, vacuum chamber 18, diffusing tube 19 is called Lavalle means for influencing) design, to utilize in rocket propulsion system/Laval nozzle means for influencing to utilize in rocket flight oxygen generation system the/suction tude of 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/air-breathing rocket atmospheric layer that flies out and enter space, closeall valve 8 make rocket chamber 7 can meet space flight requirement/using explosive under the condition that can control bursting strength as rocket propellant.

4. air-breathing duct-------1 piece of head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in many, air-breathing duct-------many pieces head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 more than 20/ of anemostat 19-------1 rocket nozzle, air-breathing duct-------many pieces head mouse 1-------many induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 more than 20/ of anemostat 19-------1 rocket nozzle, air-breathing duct-------many pieces head mouse 1-------many induction chamber 4-----many Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 more than 20/ of anemostat 19-------1 rocket nozzle, air-breathing duct-------many pieces head mouse 1-------many induction chamber 4-----many Laval nozzle 5------many anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 more than 20/ of anemostat 19-------1 rocket nozzle,1 rocket nozzle,11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injectors, 11-----1 stamping the suction 16-----1 ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, 11 points to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- 1 head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket multiple suction chamber 4-----1-----1 of laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4 ----- laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket more than 1-----4 ----- multiple suction chamber laval nozzle multiple diffusion tube 5-----6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11-----1 stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13-----1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber 19-----1 rocket nozzle 20 diffusion tube.

5. single outer air-breathing duct-------1 piece of head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10, a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 the single outer air-breathing duct of an anemostat 19-------1 rocket nozzle 20/-------many pieces head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10, a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 the single outer air-breathing duct of an anemostat 19-------1 rocket nozzle 20/-------many pieces head mouse 1-------many induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10, a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 the single outer air-breathing duct of an anemostat 19-------1 rocket nozzle 20/-------many pieces head mouse 1-------many induction chamber 4-----many Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10, a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 the single outer air-breathing duct of an anemostat 19-------1 rocket nozzle 20/-------many pieces head mouse 1-------many induction chamber 4-----many Laval nozzle 5------many anemostat 6-------1 fuel adding point 10,1 rocket nozzle,11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injectors, 11-----1 stamping the suction 16-----1 ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, 11 points to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- 1 head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket multiple suction chamber 4-----1-----1 of laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4 ----- laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket more than 1-----4 ----- multiple suction chamber laval nozzle multiple diffusion tube 5-----6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11-----1 stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13-----1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber 19-----1 rocket nozzle 20 diffusion tube.

6. air-breathing duct and many outer air-breathing duct-------1 piece of head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in many, air-breathing duct and many outer air-breathing duct-------many pieces head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 more than 20/ of anemostat 19-------1 rocket nozzle, air-breathing duct and many outer air-breathing duct-------many pieces head mouse 1-------many induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 more than 20/ of anemostat 19-------1 rocket nozzle, air-breathing duct and many outer air-breathing duct-------many pieces head mouse 1-------many induction chamber 4-----many Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 more than 20/ of anemostat 19-------1 rocket nozzle,1 rocket nozzle,11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injectors, 11-----1 stamping the suction 16-----1 ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, 11 points to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- 1 head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket multiple suction chamber 4-----1-----1 of laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4 ----- laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket more than 1-----4 ----- multiple suction chamber laval nozzle multiple diffusion tube 5-----6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11-----1 stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13-----1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber 19-----1 rocket nozzle 20 diffusion tube.

7. air-breathing duct-------1 piece of head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in two branch fork dendroids, air-breathing duct-------many pieces head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 anemostat 19-------1 rocket nozzle 20/ two branch fork dendroids, air-breathing duct-------many pieces head mouse 1-------many induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 anemostat 19-------1 rocket nozzle 20/ two branch fork dendroids, air-breathing duct-------many pieces head mouse 1-------many induction chamber 4-----many Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 anemostat 19-------1 rocket nozzle 20/ two branch fork dendroids,1 rocket nozzle,11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injectors, 11-----1 stamping the suction 16-----1 ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, 11 points to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- 1 head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket multiple suction chamber 4-----1-----1 of laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4 ----- laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket more than 1-----4 ----- multiple suction chamber laval nozzle multiple diffusion tube 5-----6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11-----1 stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13-----1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber 19-----1 rocket nozzle 20 diffusion tube.

8. air-breathing duct-------1 piece of head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in two branch fork dendroids, air-breathing duct-------many pieces head mouse 1-------1 induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 anemostat 19-------1 rocket nozzle 20/ two branch fork dendroids, air-breathing duct-------many pieces head mouse 1-------many induction chamber 4-----1 Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 anemostat 19-------1 rocket nozzle 20/ two branch fork dendroids, air-breathing duct-------many pieces head mouse 1-------many induction chamber 4-----many Laval nozzle 5------1 anemostat 6-------1 fuel adding point 10 in a fuel adding point 11-------1 punching press air intake duct 16------1 igniting place 9------1 oxygen air intake duct 13-----1 oxygen generating plant 14-------1 non-oxygen discharge pipe 15------1 rocket chamber 7-------1 Laval nozzle 17-----1 vacuum chamber 18------1 anemostat 19-------1 rocket nozzle 20/ two branch fork dendroids,1 rocket nozzle,11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injectors, 11-----1 stamping the suction 16-----1 ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, 11 points to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel,11 ----- stamping multiple points to fuel the suction 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 rocket nozzle of more than 20 / inside inspiratory bypass ----- head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- 1 head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket a suction chamber 4-----1-----1 a laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket multiple suction chamber 4-----1-----1 of laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4 ----- laval nozzle 5-----1 diffusion tube 6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket more than 1-----4 ----- multiple suction chamber laval nozzle multiple diffusion tube 5-----6-----1 point to fuel 10, 11-----1 to fuel a stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11-----1 stamping the suction 16-----1 ignition in 9-----1 oxygen inhalation tube 13-----1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16-----1 ignition in 9-----1 oxygen inhalation tube 13 14-----1-----1 oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 oxygen inhalation tube 1 oxygen generating equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group)----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition in 9-----13-----1 psa oxygen inhalation tube equipment 14-----1 the oxygen outlet pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14-----1 more oxygen generation equipment are not oxygen discharge pipe 15-----1 the rocket combustion chamber 7-----1 laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7-----1 laval nozzle 17-----1 vacuum chamber 18-----1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- a vacuum chamber 1 diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10, 11 points to fuel to fuel ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber diffusion tube 19-----1 the rockets within 20 / single suction nozzle bypass (with laval nozzle group) ----- more than the head small rocket 1 ----- multiple suction chamber 4-----5 ----- laval nozzle multiple diffusion tube 6-----10 points to fuel, fuel injection point 11 ----- stamping multiple air suction pipe 16 ----- multiple ignition of 9 ----- oxygen inhalation tube 13-----14 ----- a multiple oxygen generation equipment are not oxygen discharge pipe 15 ----- multiple rocket combustion chamber 7 ----- laval nozzle 17-----18 ----- more than a vacuum chamber 19-----1 rocket nozzle 20 diffusion tube.

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.