CN105041508A

CN105041508A - Working method of Laval nozzle effect superposition ram oxygen production rocket

Info

Publication number: CN105041508A
Application number: CN201510425003.4A
Authority: CN
Inventors: 杜善骥
Original assignee: Individual
Current assignee: Individual
Priority date: 2015-07-17
Filing date: 2015-07-17
Publication date: 2015-11-11

Abstract

Zero-speed take-off, active air breathing and fueling of a Laval effect superposition ram oxygen production rocket are achieved after a small rocket located on the head portion drives a jet air-breathing device, all valves 8 are closed after the rocket enters the space, then the rocket flies through combustion of traditional liquid hydrogen and liquid oxygen and returns to the atmosphere after work is done in the space, and the small rocket located on the head portion is ignited again to start the Laval superposition air-breathing rocket to return to the ground. The Laval superposition air-breathing rocket can be repeatedly used. The working principle of the Laval superposition air-breathing rocket is based on the fact that an American engineer uses a Laval nozzle with one end provided with positive pressure and the other end provided with negative pressure, so that a ping pong ball reaches the supersonic velocity to break a racket (please refer to the part about Laval nozzle in the substantive examination reference material), flames of a rocket nozzle are made to enter a Laval effect device to generate hypersonic-velocity jet flames, and then the rocket flies at a higher speed and can achieve ram air breathing and oxygen production in flight.

Description

Laval nozzle effect superposition punching press oxygen rocket method of work

Technical field

Lavalle effect superposition punching press 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

Laval nozzle effect superposition punching press oxygen rocket can take off in zero-speed, active inspiration and filling and fuel mix 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< or, with outer air-breathing duct 3>, induction chamber 4, Laval nozzle 5, diffusing tube 6 is called the 1st cover jet suction means) to light a fire or with the flame ignition of Laval nozzle 5 in igniting place 9, burn in the typhon mouth of diffusing tube 6 (or haul diffusing tube 6 and set up a firing chamber and a Laval nozzle, the rocket of Laval nozzle is sprayed in diffusing tube 15), the flame flow produced sprays into the 2nd cover 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) rocket fuel of annotating, light a fire or the flame ignition of diffusing tube 6 in igniting place 18, burn in firing chamber 7, 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, filling rocket fuel, diffusing tube 6, enter diffusing tube 15, another part air is divided into two-way, one tunnel is through outer suction port 17, outer air-breathing duct 16, fueling again, enter in diffusing tube 15, another road imports in the typhon mouth of diffusing tube 15 through punching press sucking pipe 19, light a fire through igniting place 18, burn in firing chamber 7, flame sprays in diffusing tube 25 through Laval nozzle 23, now vacuum chamber can produce vacuum (please read the sparger part in examination as to substances reference) Laval nozzle 23 and can produce Laval nozzle effect, malleation comes from firing chamber 7, negative pressure comes from vacuum chamber, flame gas fails to be convened for lack of a quorum and to spray through rocket nozzle with higher speed, what rocket was flown is faster, Laval nozzle effect 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 used in rocket propulsion system, make the faster of rocket flight.And awing can oxygen, closeall valve 8 when entering space, traditional liquid hydrogen and liquid oxygen combustion manner is used to fly, at the complete reentry of space work, head mouse is lighted a fire again, start Laval nozzle effect superposition punching press oxygen rocket and return to ground, this rocket is can the rocket of Reusability.

The appended drawings show

fig. 1many interior air-breathing duct Laval nozzle effect superposition punching press oxygen rockets figure, as Fig. 1shown in, 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 pass from head mouse 1 inside, after head mouse (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), air sucks through 4 interior air-breathing ducts by vacuum, filling rocket fuel is pushed in diffusing tube 6 by the flame of Laval nozzle 5, after igniting place 9 is lighted a fire, burn the high velocity air produced in the typhon mouth of diffusing tube 6, spray into diffusing tube 15 (and Open valve 8), this procreative vacuum (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, the flame that fueling is diffused pipe 6 pushes 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 can in this two air inlet mouth of pipe places filling rocket fuels and igniting), air and rocket fuel are imported in the middle part of 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 to burn, flame sprays in diffusing tube 25 through Laval nozzle 23, now vacuum chamber 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 flame sprays with higher speed from rocket nozzle through diffusing tube 25, make the faster of rocket flight, when the stamping pressure that rocket speed produces, when can meet oxygen liquefaction oxygen condition, open two oxygen sucking pipes 20 (oxygen sucking pipe can be designed to Laval nozzle shape), the air entered is compressed further, open the valve 8 on these two pipes), the air be stamped enters oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity, be discharged to below rocket nozzle through non-oxygen discharge tube 22 and discharge.

fig. 2that many interior air-breathing ducts superpose punching press oxygen rocket with single outer air-breathing duct Laval nozzle effect figure, as Fig. 2shown in, 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 (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 and outer air-breathing duct 3 by vacuum, pushed in diffusing tube 6 by the flame of Laval nozzle 5, after filling rocket fuel is lighted, burn the high velocity air produced in the typhon mouth of diffusing tube 6, spray into diffusing tube 15 (and Open valve 8), the outer procreative vacuum of air-breathing duct 16 of this process (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, adding the flame that rocket fuel is diffused pipe 6 pushes in induction chamber 7, another part air (can by these two pipe design Laval nozzle shapes through two punching press sucking pipes 19, 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), enter the middle part of diffusing tube 15, after igniting place 18 is lighted a fire, converge to be pressed in firing chamber 7 with the mixed material in diffusing tube 15 and burn, flame sprays in diffusing tube 25 through Laval nozzle 23, now vacuum chamber 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 flame sprays with higher speed from rocket nozzle through diffusing tube 25, make the faster of rocket flight, when the stamping pressure that rocket speed produces, when can meet oxygen liquefaction oxygen condition, open two oxygen sucking pipes 20 (oxygen sucking pipe can be designed to Laval nozzle shape), the air entered is compressed further, open the valve 8 on these two pipes), the air be stamped enters oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity, be discharged to below rocket nozzle through non-oxygen discharge tube 22 and discharge.

fig. 3it is single outer air-breathing duct Laval nozzle effect superposition punching press oxygen rocket figure, as accompanying drawing 3shown in, after head mouse (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, filling rocket fuel is pushed in diffusing tube 6 by the flame of Laval nozzle 5, after igniting place 9 is lighted a fire, burn the high velocity air produced in the typhon mouth of diffusing tube 6, spray into diffusing tube 15 (and Open valve 8), this procreative vacuum (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, being diffused pipe 6 after fueling igniting pushes 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 can this air inlet mouth of pipe place filling rocket fuel and igniting), air and rocket fuel are imported in the middle part of 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 to burn, flame sprays in diffusing tube 25 through Laval nozzle 23, now vacuum chamber 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 flame sprays with higher speed from rocket nozzle through diffusing tube 25, make the faster of rocket flight, when the stamping pressure that rocket speed produces, when can meet oxygen liquefaction oxygen condition, open two oxygen sucking pipes 20 (oxygen sucking pipe can be designed to Laval nozzle shape), the air entered is compressed further, open the valve 8 on these two pipes), the air be stamped enters oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity, be discharged to below rocket nozzle through non-oxygen discharge tube 22 and discharge.

fig. 4it is single interior air-breathing duct (band nozzle group) Laval nozzle effect superposition punching press oxygen rocket figure, as Fig. 4shown in, 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 (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, filling rocket fuel is pushed in diffusing tube 6 by the flame of Laval nozzle 5 (nozzle group), after igniting place 9 is lighted a fire, burn the high velocity air 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), vacuum is by shouting 17 by air intake by outer air-breathing duct 16 and air-breathing, the flame that filling rocket fuel is diffused pipe 6 pushes 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 La Er nozzle-like, as needed can annotate at the suction port place of these two Laval nozzles rocket fuel and igniting), air and rocket fuel are imported in the middle part of 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 to burn, flame 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 flame sprays with higher speed from rocket nozzle through diffusing tube 25, make the faster of rocket flight, when the stamping pressure that rocket speed produces, when can meet oxygen liquefaction oxygen condition, open two oxygen sucking pipes 20 (oxygen sucking pipe can be designed to Laval nozzle shape), the air entered is compressed further, open the valve 8 on these two pipes), the air be stamped enters oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity, be discharged to below rocket nozzle through non-oxygen discharge tube 22 and discharge.

fig. 5it is air-breathing duct Laval nozzle effect superposition punching press oxygen rocket in many branch fork dendroids figure, as Fig. 5shown in, 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 at the head mouse 1 afterbody annular wall around interior air-breathing duct 2, after head mouse (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 forks 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 sucks, filling rocket fuel is pushed in diffusing tube 6 by the flame of Laval nozzle 5 (nozzle group), after igniting place 9 is lighted a fire, burn the high velocity air 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), vacuum is by shouting 17 by air intake by outer air-breathing duct 16 and air-breathing, the flame that filling rocket fuel is diffused pipe 6 pushes 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 La Er nozzle-like, as needed can annotate at the suction port place of these two Laval nozzles rocket fuel and igniting), air and rocket fuel are imported in the middle part of 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 to burn, flame 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 flame sprays with higher speed from rocket nozzle through diffusing tube 25, make the faster of rocket flight, when the stamping pressure that rocket speed produces, when can meet oxygen liquefaction oxygen condition, open two oxygen sucking pipes 20 (oxygen sucking pipe can be designed to Laval nozzle shape), the air entered is compressed further, open the valve 8 on these two pipes), the air be stamped enters oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity, be discharged to below rocket nozzle through non-oxygen discharge tube 22 and discharge.

fig. 6that Laval nozzle effect superposition punching press oxygen rocket installation and name of parts are carefully shown.

Embodiment

Its composition of Lavalle effect 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, interior air-breathing duct horn mouth 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.

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 (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 forks 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 air-breathing duct 2 in many branch fork dendroids also can be strengthened the injection intensity of Laval nozzle 5 (nozzle group) by vacuum while sucking, pushed in diffusing tube 6 at fuel adding point 10 and fuel adding point 11 rocket fuel of annotating by the flame of Laval nozzle 5 (nozzle group), after igniting place 9 is lighted a fire, the high velocity air produced that burns in the typhon mouth of diffusing tube 6 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 is by shouting 17 by air intake by outer air-breathing duct 16 and air-breathing, push diffusing tube 15 enter in firing chamber 7 at annotate flame that rocket fuel is diffused pipe 6 of fuel adding point 13 and fuel adding point 14, 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, as needed can annotate at the suction port place of these two Laval nozzles rocket fuel and igniting), air and rocket fuel are imported in the middle part of 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 to burn, flame 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 flame sprays with higher speed from rocket nozzle through diffusing tube 25, make the faster of rocket flight, when the stamping pressure that rocket speed produces, when can meet oxygen liquefaction oxygen condition, open two oxygen sucking pipes 20 (oxygen sucking pipe can be designed to Laval nozzle shape), the air entered is compressed further, open the valve 8 on these two pipes), the air be stamped enters oxygen generating plant 21 oxygen through oxygen sucking pipe 20, non-oxidising gas after oxygen and impurity, be discharged to below rocket nozzle through non-oxygen discharge tube 22 and discharge.

You can take off in zero-speed by effect Bearing score effect superposition punching press oxygen rocket, active inspiration and fueling are that something or somebody to fall back on portion mouse drives jet suction means to complete, closeall valve 8 when entering space, use traditional liquid hydrogen and the flight of liquid oxygen combustion manner, at the complete reentry of space work, head mouse is lighted a fire again, start Lavalle superposition air-breathing rocket and return to ground, Lavalle superposition air-breathing 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), the flame of rocket nozzle is made to enter Lavalle means for influencing, produce hypersonic jet flames, make the speed of rocket flight faster, there are punching press air-breathing and oxygen separating function awing.

Claims

1. Laval nozzle effect superposes equipment and the parts of punching press 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, rear portion rocket chamber 7, valve 8, igniting place 9, fuel adding point 10, fuel adding point 11, interior air-breathing duct horn mouth 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, the Laval nozzle effect that Laval nozzle 23 is produced/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, in the rocket air-breathing that the rocket zero-speed that the vacuum produced uses is taken off, the flame of Lavalle 5 is that diffusing tube 6 typhon mouth material igniting/oxygen sucking pipe 20 accesses from outer air-breathing duct 16 and is designed to Laval nozzle shape.

3. diffusing tube 6 typhon mouth one end is as fuel chambers/connect diffusing tube 6 typhon mouth afterbody to set up a fuel chambers and a Laval nozzle, the flame of Laval nozzle is sprayed in diffusing tube 6, make the power of rocket more powerful/flame of diffusing tube 6 sprays into the power of power/uses head mouse that the vacuum produced in diffusing tube 15 is the initial flight air-breathing of superposition ram rocket (need with traditional rocket of liquid oxygen) as driving jet suction means.

4. diffusing tube 6 typhon mouth one end is as fuel chambers/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/flame of diffusing tube 6 sprays into the vacuum that produces in the diffusing tube 15 position setting/multiple head mouse pipeline communication as igniting place 18 of the power/in diffusing tube 15 of the initial flight air-breathing of superposition ram rocket, upper level is vented as secondary air-breathing, multipole pressurization system.

5. single interior air-breathing duct (band Bearing score nozzle)--------1 piece of head mouse 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouses 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------1 fuel adding point 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16,A suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,A suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, a suction hole 17-----many igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, a suction hole 17-----many igniting place 18----many punching press air intake ducts 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single interior air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 single interior air-breathing duct of an anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ (band Bearing score nozzle)--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,

6. single outer air-breathing duct--------1 piece of head mouse 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouses 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------1 fuel adding point 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16,A suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,A suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, a suction hole 17-----many igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, a suction hole 17-----many igniting place 18----many punching press air intake ducts 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 single outer air-breathing duct of an anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,A suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 single outer air-breathing duct of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 single outer air-breathing ducts of a rocket nozzle 26-------1 rocket envelope 27/--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 rocket nozzle more than 26/ outer air-breathing duct--------1 piece of head mouse 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding points 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouses 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding points 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16,A suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------1 Laval nozzle 5------1 fuel adding points 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------1 fuel adding points 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16,A suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------1 outer air-breathing duct 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, a suction hole 17-----many igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,A suction hole 17-----many igniting place 18----many punching press air intake ducts 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, a suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,Suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 rocket nozzle 26.

7. air-breathing culvert and multiple outer air-breathing duct--------1 piece of head mouse 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in many, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouses 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16,Air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,Air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----many punching press air intake ducts 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 of air-breathing culvert and multiple outer air-breathing duct in suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,Air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing culvert and multiple outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing culvert and single outer air-breathing duct--------1 piece of head mouse 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many more than 26/ of anemostat 25-----1 rocket nozzle, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and single outer air-breathing duct--------many pieces of head mouses 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16,Air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16,Air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,Air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----many punching press air intake ducts 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 of air-breathing culvert and single outer air-breathing duct in suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing culvert and single outer air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 more than 27/ of rocket nozzle 26-------1 rocket envelope, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,Suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 rocket nozzle 26.

8. air-breathing duct--------1 piece of head mouse 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in two branch fork dendroids, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouses 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16,Air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,Air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----many punching press air intake ducts 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,Air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 rocket nozzle 26.

9. air-breathing duct--------1 piece of head mouse 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in many branch fork dendroids, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouses 1---------1 induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------1 Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------1 fuel adding point 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16,Air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, a fuel adding 11-----1 anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, fuel adding 11-----many anemostat 6------1 fuel adding point 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------1 outer air-breathing duct 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope 27/ two branch fork dendroids, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,Air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----1 igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----1 punching press air intake duct 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----many punching press air intake ducts 19-----1 fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----1 Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16,Air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in a suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------1 anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, air-breathing duct--------many pieces of head mouse 1---------many induction chamber 4------many Laval nozzle 5------many fuel adding points 10 in suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 rocket nozzle 26-------1 rocket envelope more than 27/ branch fork dendroid, fuel adding 11-----many anemostat 6------many fuel adding points 13, fuel adding point 14-------many outer air-breathing ducts 16, suction hole 17-----many igniting place 18----many punching press air intake duct 19-----many fuel chambers 7-----many Laval nozzle 23-----1 vacuum chamber 24-------many anemostat 25-----1 rocket nozzle 26.

10. your effect Bearing score effect superposition punching press oxygen rocket can take off in zero-speed, active inspiration and fueling are that something or somebody to fall back on portion mouse drives jet suction means to complete, closeall valve 8 when entering space, use traditional liquid hydrogen and the flight of liquid oxygen combustion manner, at the complete reentry of space work, head mouse is lighted a fire again, start Lavalle superposition air-breathing rocket and return to ground, Lavalle superposition air-breathing 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), the flame of rocket nozzle is made to enter Lavalle means for influencing, produce hypersonic jet flames, make the speed of rocket flight faster, there are punching press air-breathing and oxygen separating function awing.