CN105134410A

CN105134410A - Operating method of detonation superposition ram propulsion and oxygen generation rocket based on Laval nozzle effect

Info

Publication number: CN105134410A
Application number: CN201510483544.2A
Authority: CN
Inventors: 杜善骥
Original assignee: Individual
Current assignee: Individual
Priority date: 2015-08-09
Filing date: 2015-08-09
Publication date: 2015-12-09

Abstract

A detonation superposition ram propulsion and oxygen generation rocket based on a Laval nozzle effect can take off at zero speed, the burning of a rocket engine can be supported by air of the atmosphere, active air breathing, fuel adding (explosives) and mixing with air are finished in a way that a jet air breathing device is driven to breathe air for two times or three times by a nose small rocket 1 (a traditional rocket which uses liquid oxygen), all valves 8 are closed when the rocket enters the space, the rocket flies in a traditional liquid hydrogen and liquid oxygen burning mode (the propulsion and oxygen generation rocket based on the Laval nozzle effect can quickly fly and has a good oxygen generation effect) and returns to the atmosphere after operation in space, and the nose small rocket 1 is ignited once again, so that the detonation superposition ram propulsion and oxygen generation rocket based on the Laval nozzle effect returns to the ground. The rocket can be reused, and the principle is that an American engineer uses the Laval nozzle effect so that a table tennis ball reaches the supersonic speed to smash a table tennis bat, and the technique of the Laval nozzle effect is applied to a rocket propulsion and oxygen generation system.

Description

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

Technical field

Detonation superposition punching press Laval nozzle effect advances and oxygen rocket method of work, relates to and belongs to aviation and space technology field.For following 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 jet passenger plane, 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 1/10.Use superposition punching press oxygen rocket method of work, the rocket manufactured can enable expense be down to 1%. to make rocket be competent at just large carrying capacity, consume oxygen in-flight few, can Preparation of oxygen be also that space flight prepares in atmospheric layer, sky and space plane and re-entry space vehicle be established oneself in an unassailable position in the business competition of space on the horizon.

Summary of the invention

Detonation superposition punching press Laval nozzle effect advances and oxygen rocket can take off in zero-speed, active inspiration, filling rocket fuel (explosive) and mix with air be something or somebody to fall back on portion mouse 1 (being need to use traditional rocket of liquid oxygen) drive the 1st overlap jet suction means (interior air-breathing duct 2 Room 4 < or, with outer air-breathing duct 3 >, induction chamber 4, Laval nozzle 5, diffusing tube 6 is called the 1st cover jet suction means) induction chamber 4 can produce vacuum (please read examination as to substances with reference to the sparger part in reference), at fuel adding point 10, fuel adding point 11 is annotated rocket fuel (explosive), to light a fire or with the flame ignition of Laval nozzle 5 in igniting place 9, in the typhon mouth of diffusing tube 6, producing detonation, (or then diffusing tube 6 afterbody sets up a firing chamber and a Laval nozzle, the detonation wave of this Laval nozzle is made to spray in diffusing tube 15, the more powerful of rocket can be made), the detonation wave produced sprays into (spraying in diffusing tube 15) the 2nd and overlaps jet suction means (suction port 17, outer air-breathing duct 16, diffusing tube 6, diffusing tube 15 is called the 2nd cover jet suction means) outer air-breathing duct 16 can produce vacuum (please read the sparger part in examination as to substances reference), at filling fire point 13, fuel adding point 14 is annotated rocket fuel (explosive), light a fire or the flame ignition of diffusing tube 6 in igniting place 18, detonation is produced in firing chamber 7, make rocket flight, when the speed of rocket enables the pressure of air punching press meet punching press condition, head mouse 1 quits work, air through interior air-breathing duct 2 (or, with outer air-breathing duct 3), induction chamber 4, enter in diffusing tube 6, another part air is through suction port 17, outer air-breathing duct 16, at fuel adding point 13, fuel adding point 14 fueling (explosive), enter in diffusing tube 15, also some air is through suction port 17, outer air-breathing duct 16, two punching press sucking pipes 19 (can be designed to Laval nozzle to sucking pipe 19 by punching press, as required fuel adding point and igniting place are set at air intlet place, and Open valve 8) import in the typhon mouth of diffusing tube 15, light a fire through igniting place 18, together enter in firing chamber 7 with the air in diffusing tube 15 and rocket fuel (explosive) and produce detonation, detonation wave sprays in diffusing tube 25 through Laval nozzle 23, vacuum chamber 24 can produce vacuum (please read the sparger part in examination as to substances reference) Laval nozzle 23 can produce Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of Laval nozzle 23 comes from firing chamber 7, negative pressure comes from vacuum chamber 24, detonation wave can spray through rocket nozzle 25 with higher speed, what rocket was flown is faster, Laval nozzle effect working principle derives from American engineer and utilizes Laval nozzle, malleation is set up in one end, the other end sets up negative pressure, make table tennis reach ultrasound velocity and smash table tennis bat (the Laval nozzle part see examination as to substances reference), this technology is used in rocket propulsion system, make the faster of rocket flight.When the stamping pressure that the speed of rocket flight enables sky oxygen produce meets oxygen liquefaction oxygen condition, open the valve 8 in oxygen sucking pipe 20 (oxygen sucking pipe front end airflow partial design becomes Laval nozzle), air is stamped to oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity are through non-oxygen discharge tube 22 (opening the valve 8 on two pipes), through vacuum chamber 24, diffusing tube 25, rocket nozzle 26 is discharged, this oxygen preparation has Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of the Laval nozzle of oxygen sucking pipe 20 front end comes from the pressure of the air that the punching press of rocket front end is come in, negative pressure comes from vacuum chamber 24, therefore Bearing score nozzle effect is just had at the Laval nozzle of oxygen sucking pipe 20 front end, the air entered can bang into oxygen in oxygen generating plant 21 with high speed, non-oxidising gas after oxygen and impurity enter vacuum chamber 24 through non-oxygen discharge tube 22, under Laval nozzle effect situation, oxygen manufacturing capacity can be more powerful.

Accompanying drawing explanation

Fig. 1 is that many interior air-breathing duct detonation superposition punching press Laval nozzle effects advance and oxygen rocket figure, as shown in Figure 1, 4 interior air-breathing ducts 2 penetrate head mouse 1 inside from the front of head mouse 1 passes to induction chamber 4, these 4 interior air-breathing ducts 2 pass from head mouse 1 inside, after head mouse 1 (being the traditional rocket need using liquid oxygen) startup work, when the flame of Laval nozzle 5 sprays into diffusing tube 6, induction chamber 4 can produce vacuum (please read the sparger part in examination as to substances reference), vacuum sucks through 4 interior air-breathing ducts 2, 10, 11 fuel adding points filling rocket fuel (explosive), pushed in diffusing tube 6 by the flame of Laval nozzle 5, to light a fire or with the flame ignition of Laval nozzle 5 in igniting place 9, detonation is produced in the typhon mouth of diffusing tube 6, spray into diffusing tube 15 (and Open valve 8), the procreative vacuum of outer air-breathing duct 16 (the sparger part in examination as to substances reference please be read), 17 are shouted by air intake by outer air-breathing duct 16 and air-breathing, 13, 14 fuel adding points filling rocket fuel (explosive) enter in firing chamber 7 through diffusing tube 15, another part air (opens the valve 8 on these two pipes through two punching press sucking pipes 19, these two pipes can be designed to Laval nozzle shape, at these two air inlet mouth of pipe place filling rocket fuels and igniting place can be set as required), air and rocket fuel are imported in the middle part of diffusing tube 15 typhon mouth, mix with the air in diffusing tube 15 and rocket fuel (explosive), in the flame ignition of igniting place 18 or diffusing tube 6, enter firing chamber 7 and produce detonation, detonation wave sprays in diffusing tube 25 through Laval nozzle 23, vacuum chamber 24 can produce the vacuum sparger of examination as to substances reference (please read part) meanwhile Laval nozzle 23 can produce Laval nozzle effect (the Laval nozzle part of examination as to substances reference please be read), when detonation wave sprays with higher speed from rocket nozzle 26 through diffusing tube 25, make the faster of rocket flight, when the stamping pressure that the speed of rocket flight enables air produce meets oxygen liquefaction oxygen condition, (oxygen sucking pipe front end airflow notch portion is designed to Laval nozzle shape to open oxygen sucking pipe 20, ) on valve 8, air is stamped to oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity are through non-oxygen discharge tube 22 (opening the valve 8 on two pipes), through vacuum chamber 24, diffusing tube 25, rocket nozzle 16 is discharged, this oxygen preparation has Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of the Laval nozzle of oxygen sucking pipe 20 front end comes from the pressure of the air that the punching press of rocket front end is come in, negative pressure comes from vacuum chamber 24, therefore Bearing score nozzle effect is just had at the Laval nozzle of oxygen sucking pipe 20 front end, the air entered can bang into oxygen in oxygen generating plant 21 with higher speed, non-oxidising gas after oxygen and impurity enter vacuum chamber 24 through non-oxygen discharge tube 22 and discharge, under Laval nozzle effect situation, oxygen manufacturing capacity can be more powerful.

Fig. 2 is that many interior air-breathing ducts superpose punching press Laval nozzle effect and advance and oxygen rocket figure with the detonation of single outer air-breathing duct, as shown in Figure 2, 4 interior air-breathing ducts 2, penetrate inside to pass (induction chamber and outer air-breathing duct fuse) from the front of head mouse 1 to outer air-breathing duct 3, after head mouse 1 (being the traditional rocket need using liquid oxygen) startup work, when the flame of Laval nozzle 5 sprays into diffusing tube 6, outer air-breathing duct 3 can produce vacuum (please read the sparger part in examination as to substances reference), air sucks through 4 interior air-breathing ducts 2 and outer air-breathing duct 3 by vacuum, at fuel adding point 10, 11 filling rocket fuel (explosive) are in the flame ignition of igniting place 9 Laval nozzle 5, detonation is produced in the typhon mouth of diffusing tube 6, detonation wave sprays into diffusing tube 15 (and Open valve 8), the procreative vacuum of outer air-breathing duct 16 (the sparger part in examination as to substances reference please be read), air is shouted 17 suctions by outer air-breathing duct 16 and air-breathing by vacuum, at fuel adding point 13, 14 filling rocket fuel (explosive) enter in firing chamber 7 through diffusing tube 15, another part air (just uses when meeting punching press suction condition through two punching press sucking pipes 19, can by these two pipe design Laval nozzle shapes, also can as required at mouth of pipe place that air enters filling rocket fuel and arrange igniting place, open the valve 8 on these two pipes), import in diffusing tube 15, in igniting place 18 or diffusing tube 6 flame ignition, mix with air with the rocket fuel (explosive) in diffusing tube 15, enter in firing chamber 7 and produce detonation, detonation wave sprays in diffusing tube 25 through Laval nozzle 23, vacuum chamber 24 can produce vacuum (please read the sparger part of examination as to substances reference) Laval nozzle 23 can produce Laval nozzle effect (please read the Laval nozzle part of examination as to substances reference), detonation wave is when diffusing tube 25 sprays from rocket nozzle 26 with higher speed, make the faster of rocket flight, when the stamping pressure that the speed of rocket flight enables air produce meets oxygen liquefaction oxygen condition, open the valve 8 on oxygen sucking pipe 20 (oxygen sucking pipe 20 front end airflow part is designed to Laval nozzle), air is stamped to oxygen generating plant 21 oxygen, non-oxidising gas after oxygen and impurity are through non-oxygen discharge tube 22 (opening the valve 8 on two pipes), through vacuum chamber 24, diffusing tube 25, rocket nozzle 26 is discharged, this oxygen preparation has Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of the Laval nozzle of oxygen sucking pipe 20 front end comes from the air that the punching press of rocket front end is come in, negative pressure comes from vacuum chamber 24 and discharges, therefore under Laval nozzle effect situation, oxygen manufacturing capacity can be more powerful.

Fig. 3 is that single outer air-breathing duct detonation superposition punching press Laval nozzle effect advances and oxygen rocket figure, as shown in Figure 3, after head mouse 1 (being the traditional rocket need using liquid oxygen) startup work, when the flame of Laval nozzle 5 sprays into diffusing tube 6, outer air-breathing duct 3 can produce vacuum (please read the sparger part in examination as to substances reference), air sucks through outer air-breathing duct 3 by vacuum, at fuel adding point 10, 11 filling rocket fuel (explosive), pushed in diffusing tube 6 by the flame of Laval nozzle 5, igniting place 9 or light a fire with Laval nozzle, detonation is produced in the typhon mouth of diffusing tube 6, detonation wave sprays into diffusing tube 15 (and Open valve 8), the procreative vacuum of outer air-breathing duct 16 (the sparger part in examination as to substances reference please be read), 17 are shouted by air intake by outer air-breathing duct 16 and air-breathing, at fuel adding point 13, 14 filling rocket fuel (explosive), in a place 18 igniting, enter in firing chamber 7, meanwhile another part air (opens the valve 8 on these two pipes through two punching press sucking pipes 19, these two pipes can be designed to Laval nozzle shape, as needs at these two air inlet mouth of pipe place filling rocket fuel < explosive > and can arrange igniting place), air and rocket fuel are imported in diffusing tube 15 typhon mouth, with the air in diffusing tube 15 and fuel mix, after igniting place 18 is lighted a fire, enter firing chamber 7 and produce detonation, detonation wave sprays in diffusing tube 25 through Laval nozzle 23, vacuum chamber 24 can produce vacuum (please read the sparger part of examination as to substances reference), Laval nozzle 23 can produce Laval nozzle effect (please read the Laval nozzle part of examination as to substances reference), when detonation wave sprays with higher speed from rocket nozzle through diffusing tube 25, make the faster of rocket flight, when the stamping pressure that the speed of rocket flight enables air produce meets oxygen liquefaction oxygen condition, (oxygen sucking pipe front end airflow partial design becomes Laval nozzle shape to open oxygen sucking pipe 20, ) on valve 8, air is stamped to oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity are through non-oxygen discharge tube 22 (opening the valve 8 on two pipes), through vacuum chamber 24, diffusing tube 25, rocket nozzle 26 is discharged, this oxygen preparation has Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of the Laval nozzle of oxygen sucking pipe 20 front end comes from the pressure of the air that the punching press of rocket front end is come in, negative pressure comes from vacuum chamber 24, therefore Bearing score nozzle effect is just had at the Laval nozzle of oxygen sucking pipe 20 front end, the air entered can bang into oxygen in oxygen generating plant 21 with higher speed, non-oxidising gas after oxygen and impurity enter vacuum chamber 24 through non-oxygen discharge tube 22 and discharge, under Laval nozzle effect situation, oxygen manufacturing capacity can be more powerful.

Fig. 4 is that single interior air-breathing duct (band nozzle group) detonation superposition punching press Laval nozzle effect advances and oxygen rocket figure, as shown in Figure 4, 1 interior air-breathing duct 2, inside is penetrated from head mouse 1 front dead center centre, pass to head mouse 1 afterbody centre, head mouse 1 afterbody Laval nozzle 5 (nozzle group), be located in the head mouse afterbody annular wall around interior air-breathing duct 2, after head mouse 1 (being the traditional rocket need using liquid oxygen) startup work, the flame of Laval nozzle 5 (nozzle group) sprays and meets at a bit with funnel-like, vacuum (principle is similar to flow eddies) can be produced in funnel, air is sucked through interior air-breathing duct 2, sprayed in diffusing tube 6 by the flame flow of Laval nozzle 5 (nozzle group), now induction chamber 4 can produce vacuum (please read the sparger part in examination as to substances reference), air also can be strengthened the injection intensity of Laval nozzle 5 (nozzle group) by vacuum while interior air-breathing duct 2 sucks, at fuel adding point 10, 11 filling rocket fuel (explosive), pushed in diffusing tube 6 by the flame of Laval nozzle 5 (nozzle group), after igniting place 9 or Laval nozzle 5 (nozzle group) igniting, detonation is produced in the typhon mouth of diffusing tube 6, spray into (and Open valve 8) in diffusing tube 15, the procreative vacuum of outer air-breathing duct 16 (the sparger part in examination as to substances reference please be read), vacuum shouts 17 by air intake by outer air-breathing duct 16 and air-breathing, at fuel adding point 13, 14 filling rocket fuel (explosive), enter in firing chamber 7 through diffusing tube 15, meanwhile another part air (opens the valve 8 on these two pipes through two punching press sucking pipes 19, these two pipes can be designed to La Er nozzle-like, according to wanting at the suction port place of these two Laval nozzles filling rocket fuel < explosive > and igniting place to be arranged), air and rocket fuel (explosive) are imported in diffusing tube 15 typhon mouth, converge with the rocket fuel in diffusing tube 15 and air, after igniting place 18 is lighted a fire, spray into firing chamber 7 and produce detonation, detonation wave sprays in diffusing tube 25 through Laval nozzle 23, now vacuum chamber 24 can produce the vacuum sparger of examination as to substances reference (please read part) meanwhile Laval nozzle 23 can produce Laval nozzle effect (the Laval nozzle part of examination as to substances reference please be read), when detonation wave sprays with higher speed from rocket nozzle 26 through diffusing tube 25, make the faster of rocket flight, when the stamping pressure that the speed of rocket flight enables air produce meets oxygen liquefaction oxygen condition, (oxygen sucking pipe 20 front end airflow place is designed to Laval nozzle shape to open oxygen sucking pipe 20, ) on valve 8, air is stamped to oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity are through non-oxygen discharge tube 22 (opening the valve 8 on two pipes), through vacuum chamber 24, diffusing tube 25, rocket nozzle 26 is discharged, this oxygen preparation has Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of the Laval nozzle of oxygen sucking pipe 20 front end comes from the pressure of the air that the punching press of rocket front end is come in, negative pressure comes from vacuum chamber 24, therefore Bearing score nozzle effect is just had at the Laval nozzle of oxygen sucking pipe 20 front end, the air entered can bang into oxygen in oxygen generating plant 21 with high speed, non-oxidising gas after oxygen and impurity enter vacuum chamber 24 through non-oxygen discharge tube 22 and discharge, under Laval nozzle effect situation, oxygen manufacturing capacity can be more powerful.

Fig. 5 is that in many branch fork dendroids, air-breathing duct detonation superposition punching press Laval nozzle effect advances and oxygen rocket figure, as shown in Figure 5, 1 interior air-breathing duct 2 penetrates inside from head mouse 1 front dead center centre and passes to head mouse 1 afterbody centre, in addition four interior air-breathing ducts 2 are inner by penetrating head mouse 1 outside the head mouse 1 front dead center heart, and meet on Centromedian interior air-breathing duct 2 in head mouse 1 inside, on the Centromedian interior air-breathing duct 2 connected with dendritic structure, head mouse 1 afterbody Laval nozzle 5 (nozzle group), be located in the head mouse 1 afterbody annular wall around interior air-breathing duct 2, after head mouse 1 (being the traditional rocket need using liquid oxygen) startup work, the flame of Laval nozzle 5 (nozzle group) sprays and meets at a bit with funnel-like, vacuum (principle is similar to flow eddies) can be produced in funnel, air air-breathing duct 2 in many branch fork dendroids is sucked, sprayed in diffusing tube 6 by the flame flow of Laval nozzle 5 (nozzle group), now induction chamber 4 can produce vacuum (please read the sparger part in examination as to substances reference), air also can be strengthened the injection intensity of Laval nozzle 5 (nozzle group) by vacuum while interior air-breathing duct 2 strengthens suction again, at fuel adding point 10, 11 filling rocket fuel (explosive), pushed in diffusing tube 6 by the flame of Laval nozzle 5 (nozzle group), after igniting place 9 is lighted a fire, detonation is produced in the typhon mouth of diffusing tube 6, detonation wave sprays into diffusing tube 15 (and Open valve 8), the procreative vacuum of outer air-breathing duct 16 (the sparger part in examination as to substances reference please be read), vacuum shouts 17 by air intake by outer air-breathing duct 16 and air-breathing, at fuel adding point 13, fuel adding point 14 is annotated rocket fuel (explosive), enter in firing chamber 7 through diffusing tube 15, meanwhile another part air (opens the valve 8 on these two pipes through two punching press sucking pipes 19, these two pipes can be designed to La Er nozzle, at the suction port place of these two Laval nozzles filling rocket fuel and igniting place can be set as required), air and rocket fuel (explosive) are imported in diffusing tube 15 typhon mouth, with the gas in diffusing tube 15 and fuel mix, after igniting place 18 is lighted a fire, push firing chamber 7 and produce detonation, detonation wave sprays in diffusing tube 25 through Laval nozzle 23, now vacuum chamber 24 can produce the vacuum sparger of examination as to substances reference (please read part) meanwhile Laval nozzle 23 can produce Laval nozzle effect (the Laval nozzle part of examination as to substances reference please be read), when detonation wave sprays with higher speed through rocket nozzle 26, make the faster of rocket flight, when the stamping pressure that the speed of rocket flight enables air produce meets oxygen liquefaction oxygen condition, open the valve 8 in oxygen sucking pipe 20 (oxygen sucking pipe front end airflow partial design becomes Laval nozzle shape), air is stamped to oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity are through non-oxygen discharge tube 22 (opening the valve 8 on two pipes), discharge through vacuum chamber 24, this oxygen preparation has Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of the Laval nozzle of oxygen sucking pipe 20 front end comes from the pressure of the air that the punching press of rocket front end is come in, negative pressure comes from vacuum chamber 24, therefore Bearing score nozzle effect is just had at the Laval nozzle of oxygen sucking pipe 20 front end, the air entered can bang into oxygen in oxygen generating plant 21 with high speed, non-oxidising gas after oxygen and impurity enter vacuum chamber 24 through non-oxygen discharge tube 22 and discharge, under Laval nozzle effect situation, oxygen manufacturing capacity can be more powerful.

Fig. 6 is that detonation superposition punching press Laval nozzle effect advances and oxygen rocket installation and name of parts are carefully shown.

Embodiment

Its composition of Lavalle effect detonation superposition punching press oxygen rocket method of work: by head mouse 1, interior air-breathing duct 2 (or, with outer suction duct 3), induction chamber 4, Laval nozzle 5, diffusing tube 6, firing chamber 7, valve 8, igniting place 9, fuel adding point 10, fuel adding point 11, Laval nozzle 12, fuel adding point 13, fuel adding point this 14, diffusing tube 15, outer air-breathing duct 16, air-breathing shouts 17, igniting place 18, punching press sucking pipe 19, oxygen sucking pipe 20, oxygen generating plant 21, non-oxygen discharge tube 22, Laval nozzle 23, vacuum chamber 24, diffusing tube 25, rocket nozzle 26, rocket envelope 27.

As shown in Figure 5, 1 interior air-breathing duct 2 penetrates inside from head mouse 1 front dead center centre and passes to head mouse 1 afterbody centre, in addition four interior air-breathing ducts 2 are inner by penetrating head mouse 1 outside the head mouse 1 front dead center heart, and meet on Centromedian interior air-breathing duct 2 in head mouse 1 inside, on the Centromedian interior air-breathing duct 2 connected with dendritic structure, head mouse 1 afterbody Laval nozzle 5 (nozzle group), be located in the head mouse 1 afterbody annular wall around interior air-breathing duct 2, after head mouse 1 (being the traditional rocket need using liquid oxygen) startup work, the flame of Laval nozzle 5 (nozzle group) sprays and meets at a bit with funnel-like, vacuum (principle is similar to flow eddies) can be produced in funnel, air air-breathing duct 2 in many branch fork dendroids is sucked, sprayed in diffusing tube 6 by the flame flow of Laval nozzle 5 (nozzle group), now induction chamber 4 can produce vacuum (please read the sparger part in examination as to substances reference), air also can be strengthened the injection intensity (namely Laval nozzle effect) of Laval nozzle 5 (nozzle group) by vacuum while interior air-breathing duct 2 strengthens suction again, at fuel adding point 10, 11 filling rocket fuel (explosive), pushed in diffusing tube 6 by the flame of Laval nozzle 5 (nozzle group), igniting place 9 is lighted a fire or the flame ignition of Laval nozzle 5, detonation is produced in the typhon mouth of diffusing tube 6, detonation wave sprays into diffusing tube 15 (and Open valve 8), the procreative vacuum of outer air-breathing duct 16 (the sparger part in examination as to substances reference please be read), vacuum shouts 17 by air intake by outer air-breathing duct 16 and air-breathing, at fuel adding point 13, fuel adding point 14 is annotated rocket fuel (explosive), enter in firing chamber 7 through diffusing tube 15 and produce detonation, detonation wave sprays in diffusing tube 25 through Laval nozzle 23, now vacuum chamber 24 can produce vacuum (please read the sparger part of examination as to substances reference), Laval nozzle 23 can produce Laval nozzle effect (please read the Laval nozzle part of examination as to substances reference), the malleation of Laval nozzle 23 comes from the detonation of firing chamber 7 generation, negative pressure comes from vacuum chamber 24, when detonation wave sprays with higher speed through rocket nozzle 26, make the faster of rocket flight, when the power of rocket punching press can meet punching press suction condition, head mouse 1 quits work, due to the speed of rocket flight, can by air punching press air-breathing duct 2 in many branch fork dendroids, Laval nozzle 12, induction chamber 4, diffusing tube 6, enter in diffusing tube 15, another part air is by suction port 17, outer air-breathing duct 16, 13, 14 fuel adding points filling rocket fuel (explosive), another part air is through outer air-breathing duct 16, suction port 17, punching press sucking pipe 19 imports in diffusing tube 15, light a fire in igniting place 18, enter detonation in rocket chamber 7, detonation wave sprays in diffusing tube 25 through Laval nozzle 23, now vacuum chamber 24 can produce the vacuum sparger of examination as to substances reference (please read part) meanwhile Laval nozzle 23 can produce Laval nozzle effect (the Laval nozzle part of examination as to substances reference please be read), the malleation of Laval nozzle 23 comes from the detonation of rocket chamber 7 generation, negative pressure comes from vacuum chamber 24, when detonation wave sprays with higher speed through rocket nozzle 26, make the faster of rocket flight, when the stamping pressure that the speed of rocket flight enables air produce meets oxygen liquefaction oxygen condition, (oxygen sucking pipe front end airflow partial design becomes Laval nozzle shape to open oxygen sucking pipe 20, ) on valve 8, air is stamped to oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity are through non-oxygen discharge tube 22 (opening the valve 8 on two pipes), through vacuum chamber 24, diffusing tube 25, rocket nozzle 26 is discharged, this oxygen preparation has Laval nozzle effect (please read the Laval nozzle part in examination as to substances reference), the malleation of the Laval nozzle of oxygen sucking pipe 20 front end comes from the pressure of the air that the punching press of rocket front end is come in, negative pressure comes from vacuum chamber 24, therefore Bearing score nozzle effect is just had at the Laval nozzle of oxygen sucking pipe 20 front end, the air entered can bang into oxygen in oxygen generating plant 21 with higher speed, non-oxidising gas after oxygen and impurity enter vacuum chamber 24 through non-oxygen discharge tube 22 and discharge, under Laval nozzle effect situation, oxygen manufacturing capacity can be more powerful.

Detonation superposition punching press Laval nozzle effect advances and oxygen rocket can take off in zero-speed, active inspiration, fuel adding (explosive) and mixing with air, that something or somebody to fall back on portion mouse 1 (need with traditional rocket of liquid oxygen) drives jet suction means to carry out 2 times or 3 air-breathings complete, closeall valve 8 when entering space, traditional liquid hydrogen and the flight of liquid oxygen combustion manner is used (to have the rocket of Laval nozzle effect propulsion functions, that can fly is faster), at the complete reentry of space work, head mouse 1 is lighted a fire again, detonation superposition punching press Laval nozzle effect propelling and oxygen rocket is made to return to ground, this rocket is can the rocket of Reusability, principle is that American engineer utilizes Laval nozzle effect, make table tennis reach ultrasound velocity and smash table tennis bat, Laval nozzle effect technology is applied in rocket propulsion and oxygen generation system.

Claims

1. detonation superposes equipment and the parts of the propelling of punching press Laval nozzle effect and oxygen rocket method of work, by head mouse 1, interior air-breathing duct 2 (or outer suction 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, fuel adding point 13, fuel adding point 14, diffusing tube 15, outer air-breathing duct 16, air-breathing shouts 17, igniting place 18, oxygen sucking pipe 20, oxygen generating plant 21, non-oxygen discharge tube 22, Laval nozzle 23, vacuum chamber 24, diffusing tube 25, rocket nozzle 26, rocket envelope 27.

2. the flame flow of Laval nozzle 23 sprays into the vacuum that in diffusing tube 25, vacuum chamber 24 produces, make the Laval nozzle effect that Laval nozzle 23 produces, Laval nozzle effect is used in rocket propulsion system, also Laval nozzle effect can be applied to other field/by non-oxygen discharge tube 22 accesses while vacuum chamber 24 makes non-oxidising gas discharge, oxygen preparation is made to have Laval nozzle effect, namely Laval nozzle effect to be used in rocket flight oxygen preparation/spray into diffusing tube 15 at diffusing tube 6 high velocity air, form vacuum and drive the 2nd inhalation methods/at fuel adding point 13, fuel adding point 14 is annotated rocket fuel/spray in diffusing tube 6 with the flame of head mouse Laval nozzle 5, the vacuum produced is used in rocket air-breathing, the flame of Laval nozzle 5 is that the fuel ignition/oxygen sucking pipe 20 of diffusing tube 6 typhon mouth accesses from outer air-breathing duct 16 and is designed to Laval nozzle shape.

3. use head mouse 1 (need with traditional rocket of liquid oxygen) as the power of driving jet suction means, the vacuum of generation is rocket air-breathing/explosive is manufactured oxygen awing as rocket fuel/rocket.

4. diffusing tube 6 typhon mouth one end is as firing chamber/connect diffusing tube 6 typhon mouth afterbody to set up a fuel chambers and a Laval nozzle, the flame of Laval nozzle is made to spray in diffusing tube 6, make the power of rocket more powerful/position setting/multiple head mouse pipeline communication of igniting place 18 in diffusing tube 15, upper level is vented as secondary air-breathing, multipole pressurization system.

5. Single suction bypass 2 (with nozzle group) within 1 head small rocket a suction chamber 4-1-1 1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1-1 more head small rocket suction chamber 4-1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass 2 (with nozzle group)1 - multiple - head small rocket suction chamber 4-1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1 - multiple inhale more head small rocket chamber 4-1 a laval nozzle multiple diffusion tube 5-6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6-15 - diffusion tube 1 inspiratory bypass 16, 17-1 ignition suction hole in 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass 2 (with nozzle group)1 - multiple - head small rocket suction chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube more than 15 - inspiratory bypass 16, 17-18-1 ignition place suction hole 1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 1 oxygen generation equipment are not oxygen discharge pipe 22-23-1 a laval nozzleA vacuum chamber 24-1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - multiple pressing suction 19 - multiple rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen inhaling more than 20-21-1 oxygen generation equipment are not oxygen discharge pipe 22-23-1 a laval nozzleA vacuum chamber 24-1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen to breathe in more than 20-21-1 oxygen generation equipment are not oxygen discharge tube more than 22 - laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass (with nozzle group) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen to breathe in more than 20-21-1 oxygen generation equipment are not oxygen discharge tube more than 22-23-24 - a vacuum chamber laval nozzle multiple diffusion tube 25-1 rocket nozzle 26 / root inside inspiratory bypass head small rocket 1-2-1 a suction chamber 4-1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 1 oxygen generation equipment are not oxygen discharge pipe22-1 a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - a suction head small rocket chamber 4-1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - multiple suction head small rocket chamber 4-1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - multiple suction head small rocket chamber 4-1 a laval nozzle multiple diffusion tube 5-6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 1 oxygen generation equipment are the oxygen outlet pipe 22-1A laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - multiple suction head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6-15 - diffusion tube 1 inspiratory bypass 16, 17-18-1 ignition place suction hole 1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - multiple suction head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube more than 15 - inspiratory bypass 16, 17-18-1 ignition place suction hole 1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - multiple suction head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to Inhale within one rocket nozzle 26 / root bypass more than 2-1 - multiple suction head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - multiple suction head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - multiple pressing suction 19 - multiple rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - multiple suction head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2 - head small rocketMultiple suction chamber 4-1-1 of laval nozzle 5 - multiple diffusion tube 6 - diffusion tube outside more than 15 to inhale bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen to breathe in more than 20-21-1 oxygen generation equipment are not oxygen discharge pipe 22-1 a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - multiple suction head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to inhale bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen to breathe in more than 20-21-1 oxygen generation equipment are not oxygen discharge tube more than 22 - laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / root inside inspiratory bypass more than 2-1 - multiple suction head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen to breathe in more than 20-21-1 oxygen generation equipment are not oxygen discharge tube more than 22-23-24 - a vacuum chamber laval nozzle multiple diffusion tube 25-26 a rocket nozzle.

6. Outside a single suction bypass head small rocket 1-----3-----1 1 laval nozzle 5-----1 diffusion tube 6-----1 diffusion tube 15-----1 the inspiratory bypass 16, 17-----1 ignition suction hole 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1-----1 a laval nozzle head small rocket 5-----1 diffusion tube 6-----1 diffusion tube 15-----1 the inspiratory bypass 16, 17-----1 ignition suction hole 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1 ----- a laval nozzle head small rocket 5-----1 diffusion tube 6-----1 the diffusion tube 15-----1 inspiratory bypass 16,Suction hole 17-----1 ignition at 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1-----1 a laval nozzle head small rocket multiple diffusion tube 5-----6-----1 diffusion tube 15-----1 the inspiratory bypass 16, 17-----1 ignition suction hole 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube 15-----1 inspiratory bypass 16, 17-----1 ignition suction hole in 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----1 oxygen generating equipment 21-----22-----1 the oxygen outlet pipe a laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1 ----- a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to breathe in the bypass 16, 17 ----- a suction hole ignition 18-----1A stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1 ----- a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to breathe in the bypass 16, 17 ----- multiple ignition suction hole 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----1 oxygen generating equipment 21-----22-----1 the oxygen outlet pipe a laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1 ----- a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to breathe in the bypass 16, 17 ----- multiple ignition suction hole 18 ----- stamping multiple suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1 ----- multiple head small rocket suction chamber a laval nozzle 5-----4-----1 multiple diffusion tube 6 ----- diffusion tube more than 15 ----- inspiratory bypass 16,Suction hole 17 ----- stamping multiple ignition in 18 to the suction 19 ----- multiple rocket fuel room 7-----1 oxygen inhaling 20-----1 oxygen generating equipment 21-----22-----1 the oxygen outlet pipe a laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to inhale bypass 16, 17 ----- multiple ignition suction hole 18 ----- stamping multiple suction 19 ----- multiple rocket fuel room 7 ----- oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to breathe in the bypass 16, 17 ----- multiple ignition suction hole 18 ----- stamping multiple suction 19 ----- multiple rocket fuel room 7 ----- oxygen to breathe in more than 20-----21-----1 oxygen generation equipment are not oxygen discharge pipe 22 ----- a laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1 ----- a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube more than 15 ----- inspiratory bypass 16,Suction hole 17 ----- stamping multiple ignition in 18 to the suction 19 ----- multiple rocket fuel room 7 ----- oxygen to breathe in more than 20-----21-----1 oxygen generation equipment are not oxygen discharge tube more than 22 ----- laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to inhale bypass 16, 17 ----- multiple ignition suction hole 18 ----- stamping multiple suction 19 ----- multiple rocket fuel room 7 ----- oxygen to breathe in more than 20-----21-----1 oxygen generation equipment are not oxygen discharge tube more than 22-----23-----24 ----- a vacuum chamber laval nozzle multiple diffusion tube 25-----1 rocket nozzle 26 / multiple inspiratory bypass head small rocket 1-----3-----1 1 laval nozzle 5-----1 diffusion tube 6-----1 diffusion tube 15-----1 the inspiratory bypass 16, 17-----1 ignition suction hole 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle breathe in 26 / multiple bypass more than 3-----1-----1 a laval nozzle head small rocket 5-----1 diffusion tube 6-----1 the diffusion tube 15-----1 inspiratory bypass 16,Suction hole 17-----1 ignition at 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle more than 26 / multiple inspiratory bypass 3-----1-----1 a laval nozzle head small rocket 5-----1 diffusion tube 6-----1 diffusion tube 15-----1 the inspiratory bypass 16, 17-----1 ignition suction hole 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket 26 / single suction nozzle bypass more than 3-----1 ----- a laval nozzle head small rocket multiple diffusion tube 5-----6-----1 diffusion tube 15-----1 the inspiratory bypass 16, 17-----1 ignition suction hole 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle breathe in 26 / multiple bypass more than 3-----1 ----- a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube 15-----1 inspiratory bypass 16,Suction hole 17-----1 ignition at 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle more than 26 / multiple inspiratory bypass 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube more than 15 ----- inspiratory bypass 16, 17-----18-----1 ignition place suction hole 1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----1 oxygen generating equipment 21-----22-----1 the oxygen outlet pipe a laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle more than 26 / multiple inspiratory bypass 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to breathe in the bypass 16, 17 ----- multiple ignition suction hole 18-----1 stamping the suction 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----1 oxygen generating equipment 21-----22-----1 the oxygen outlet pipe a laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle breathe in 26 / multiple bypass more than 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube more than 15 ----- inspiratory bypass 16, 17 ----- multiple ignition suction hole 18 ----- stamping multiple air suction pipe 19-----1 rocket fuel room 7-----1 oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle more than 26 / multiple inspiratory bypass 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to inhale bypass 16, 17 ----- multiple ignition suction hole 18 ----- multiple pressing suction 19 ----- multiple rocket fuel room 7-----1 oxygen inhaling 20-----1 oxygen generating equipment 21-----22-----1 the oxygen outlet pipe a laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle more than 26 / multiple inspiratory bypass 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to breathe in the bypass 16, 17 ----- multiple ignition suction hole 18 ----- stamping multiple suction 19 ----- multiple rocket fuel room 7 ----- oxygen inhaling 20-----21-----1 oxygen generation equipment are 1 non oxygen discharge pipe 22-----1 laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle breathe in 26 / multiple bypass more than 3-----1 ----- a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube more than 15 ----- inspiratory bypass 16, 17 ----- multiple ignition suction hole 18 ----- stamping multiple air suction pipe 19 ----- multiple rocket fuel room 7 ----- oxygen to breathe in more than 20-----21-----1 oxygen generation equipment are not oxygen discharge pipe 22-----1 a laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle more than 26 / multiple inspiratory bypass 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to inhale bypass 16, 17 ----- multiple ignition suction hole 18 ----- stamping multiple suction 19 ----- multiple rocket fuel room 7 ----- oxygen to breathe in more than 20-----21-----1 oxygen generation equipment are not oxygen discharge tube more than 22 ----- laval nozzle 23-----24 ----- a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle more than 26 / multiple inspiratory bypass 3-----1-----1 a laval nozzle head small rocket 5 ----- multiple diffusion tube 6 ----- diffusion tube outside more than 15 to breathe in the bypass 16, 17 ----- multiple ignition suction hole 18 ----- stamping multiple suction 19 ----- multiple rocket fuel room 7 ----- oxygen to breathe in more than 20-----21-----1 oxygen generation equipment are not oxygen discharge tube more than 22-----23-----24 ----- a vacuum chamber laval nozzle multiple diffusion tube 25-----26 a rocket nozzle.

7. Two branches fork dendritic inspiratory bypass group (with a nozzle) 2-1 head small rocket a suction chamber 4-1-1 1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1-1 more head small rocket suction chamber 4-1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass 2 (with nozzle group)1 - multiple - head small rocket suction chamber 4-1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber 4-1 a laval nozzle multiple diffusion tube 5-6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6-15 - diffusion tube 1 inspiratory bypass 16,Suction hole 17-1 ignition at 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube more than 15 - inspiratory bypass 16, 17-18-1 ignition place suction hole 1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe 1 laval nozzle 23-1 vacuum chamber-1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to inhale bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to inhale bypass 16, 17 - multiple ignition suction hole 18 - multiple pressing suction 19 - multiple rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen inhaling 20-21-1 1 oxygen generation equipment are not oxygen discharge pipe 22-A laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle more than 26 / multiple inspiratory bypass 3-1 - multiple suction head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6-15 - multiple diffusion tube outer inspiratory bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen to breathe in more than 20-21-1 oxygen generation equipment are not oxygen discharge pipe 22-1 a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - multiple pressing suction 19 - multiple rocket fuel room 7-1 - more oxygen to breathe in 20 psa equipment More than 21 - the oxygen outlet pipe more than 22-23-24 - a vacuum chamber laval nozzle 1 diffusion tube 25 to 1 rocket nozzle 26 / two branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen inhaling more than 20-21-1 oxygen generation equipment are not oxygen discharge tube more than 22-23-24 - a vacuum chamber of laval nozzle multiple diffusion tube 25-26 a rocket nozzle.

More than 8 branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 head small rocket a suction chamber 4-1-1 1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1-1 more head small rocket suction chamber 4-1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber 4-1 laval nozzle 5-1 diffusion tube 6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with the nozzle) 2) - more than the head small rocket multiple suction chamber 4-1-1 of laval nozzle multiple diffusion tube 5-6-1 diffusion tube 15-1 the inspiratory bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6-15 - diffusion tube 1 inspiratory bypass 16, 17-18-1 ignition place suction hole 1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23 - a vacuum chamber 24-1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to inhale bypass 16, 17-1 ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to inhale bypass 16, 17 - multiple ignition suction hole 18-1 stamping the suction 19-1 rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube more than 15 - inspiratory bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple air suction pipe 19-1 rocket fuel room 7-1 oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6-15 - multiple diffusion tube outer inspiratory bypass 16, 17 - multiple ignition suction hole 18 - multiple pressing suction 19 - multiple rocket fuel room 7-1 oxygen inhaling 20-1 oxygen generating equipment 21-22-1 the oxygen outlet pipe a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to inhale bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen inhaling 20-21-1 oxygen generation equipment are 1 non oxygen discharge pipe 22-1 laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6-Breathe in multiple diffusion tube outside more than 15 to bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen to breathe in more than 20-21-1 oxygen generation equipment are not oxygen discharge pipe 22 - a laval nozzle 23-24 - a vacuum chamber 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen to breathe in more than 20-21-1 oxygen generation equipment are not oxygen discharge tube more than 22-23-24 - a vacuum chamber laval nozzle 1 diffusion tube 25 to 1 rocket nozzle 26 / branch fork dendritic inspiratory bypass group (with a nozzle) 2-1 - multiple inhale more head small rocket chamber a laval nozzle 5-4-1 multiple diffusion tube 6 - diffusion tube outside more than 15 to breathe in the bypass 16, 17 - multiple ignition suction hole 18 - stamping multiple suction 19 - multiple rocket fuel room 7 - oxygen inhaling more than 20-21-1 oxygen generation equipment are not oxygen discharge tube more than 22-23-24 - a vacuum chamber of laval nozzle multiple diffusion tube 25-26 a rocket nozzle.

9. your effect Bearing score effect detonation superposition punching press oxygen rocket can take off in zero-speed, active inspiration and filling and fuel mix with air, that something or somebody to fall back on portion mouse 1 (need with traditional rocket of liquid oxygen) drives jet suction means to complete, closeall valve 8 when entering space, traditional liquid hydrogen and the flight of liquid oxygen combustion manner is used (to have the rocket of Laval nozzle effect propulsion functions, that can fly is faster), at the complete reentry of space work, head mouse is lighted a fire again, start Lavalle effect detonation superposition punching press oxygen rocket and return to ground, this rocket is can the rocket of Reusability, 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), Laval nozzle effect technology is applied in rocket propulsion system, make the speed of rocket flight faster, there is punching press air suction function awing.

10. the working principle of Laval nozzle effect 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), Laval nozzle effect technology is applied in rocket propulsion system, Laval nozzle effect technology is applied in the oxygen manufacture of rocket in-flight.