CN102556360B - Orbit accelerating airplane capable of completing lift-off of two-stage rocket spacecraft with two-stage moving platforms - Google Patents
Orbit accelerating airplane capable of completing lift-off of two-stage rocket spacecraft with two-stage moving platforms Download PDFInfo
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- CN102556360B CN102556360B CN201210024472.1A CN201210024472A CN102556360B CN 102556360 B CN102556360 B CN 102556360B CN 201210024472 A CN201210024472 A CN 201210024472A CN 102556360 B CN102556360 B CN 102556360B
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management
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Abstract
The invention relates to an orbit accelerating airplane capable of completing lift-off of a two-stage rocket spacecraft with two-stage moving platforms, which comprises an orbit, an orbit moving platform, an airplane platform and the two-stage rocket spacecraft, and is characterized in that the orbit moving platform and the airplane platform complete start, acceleration and lift-off by means of different power sources and pass through a troposphere to enter a stratosphere, and a relaying launch means of sending the spacecraft by a rocket in the stratosphere is realized. Compared with the prior art, the orbit accelerating airplane has the notable advantages that fuels of a jet engine are saved, the rocket is small in size and low in cost, launch is less limited by a launch site, the weather and the climate, a launch window can be selected, the orbit moving platform and the airplane platform can bear various spacecrafts and is reusable and the like, thereby having quite good use value.
Description
One, technical field:
The present invention relates to space technology, particularly relate to the orbit accelerating airplane that a kind of two-stage motion platform completes the lift-off of two-stage rocket spacecraft.
two, background technology:
The theory that the three-stage rocket relay boosting spacecraft that father's Tsiolkovsky of space flight is founded enters space, become design, the design of existing space technology, the basic model of practice, but, along with extension and the expansion of the mankind to cosmic space exploration and utilization, to transmitting frequency, scale, the distance of going deep into space and return etc., all producing the comprehensive demand of matter, amount, technical risk and cost.Prior art is faced with rocket volume and the boosting power limit, launch site addressing, weather, meteorological follow, many many-sided restrictions such as accurate assurance of launch window.
three, summary of the invention:
The object of the invention is the limitation for above demand and prior art, provide a kind of cost two-stage motion platform low, reusable, that can select and chase launch window to complete the orbit accelerating airplane of two-stage rocket spacecraft lift-off.
The object of the invention is to be achieved through the following technical solutions:
Two-stage motion platform completes an orbit accelerating airplane for two-stage rocket spacecraft lift-off, and it comprises track, orbiting motion platform, aircraft platform and two-stage rocket spacecraft, is characterized in that by orbiting motion platform, aircraft platform, the interim relay campaign of two-stage rocket is transmitted operation spacecraft is sent into planned orbit, and the rocket dress that its two-stage rocket spacecraft integral body is anchored on aircraft platform by aircraft platform negative pressure disconnecting gear is taken in storehouse, aircraft platform is anchored on orbiting motion platform by orbiting motion platform negative pressure disconnecting gear, pack up alighting gear, orbiting motion platform accelerates fast linear running along track under self power system and the traction of aircraft platform jet engine dual dynamic, when its running velocity surmounts aircraft platform takeoff speed, orbiting motion platform negative pressure disconnecting gear is opened, let aircraft platform fly away and take off, aircraft platform dependence self jet engine power carries rocket dress and takes the two-stage rocket spacecraft acceleration flight in storehouse and climb, to in advection layer during ceiling altitude, select the optimum transmit window of two-stage rocket spacecraft, start the jet engine running of two-stage rocket spacecraft, when two-stage rocket spacecraft flight power surmounts aircraft platform flying speed, aircraft platform is aimed at the flight of the launch window elevation angle, and the differential force that two-stage rocket spacecraft and aircraft platform form is opened aircraft platform negative pressure disconnecting gear, let two-stage rocket spacecraft fly away, enter programmed remote control flight, aircraft platform is selected the conventional landing in suitable airport.
Above-described track is ray shape, double rail type, for orbiting motion platform, accelerates, is decelerated to dedicated track out of service.
Described orbiting motion platform is to have autonomous active power system, by 3 orbiting motion platform negative pressure disconnecting gears of front triangle, fastening and carry aircraft platform, acceleration and discharge aircraft platform, Orbiting streamline contour, high-performance express locomotive.
The cabin Position Design of described aircraft platform is that top is open, circular arc flute profile rocket dress fastening by aircraft platform negative pressure disconnecting gear and that carry two-stage rocket spacecraft is taken storehouse, aircraft platform cockpit is arranged at fuselage head below, rudder fin is set to outer Zhang Shuanyi, the special-shaped aircraft that the jet engine of take is power.
The alighting gear of described aircraft platform is packed up after aircraft platform is anchored on orbiting motion platform, to the aerial mission overall process that completes aircraft platform, before landing, opens and puts, in conventional airfield runway landing.
Described aircraft platform, as aerospace master, carries and lets fly away three grades, one-stage rocket spacecraft, spacecrafts other forms and function, different orbits.
The orbit accelerating airplane that two-stage motion platform of the present invention completes two-stage rocket spacecraft lift-off compared with prior art, has following outstanding advantages:
1, to there is the dual dynamic source of the orbiting motion platform of powerful autonomous dynamic and the aircraft platform of jet engine power, promote to take off and complete to pass through convective zone and part advection layer, in the advection layer that minimum and terrestrial gravitation reduces at air resistance, let booster-missile combination spacecraft fly away, the first order that replaces traditional three-stage rocket that power consumption is maximum, volume is maximum, risk is maximum, makes that Spacecraft Launch is safer, environmental protection, cost be lower.
2,, by two-stage motion platform carrying transmitting two-stage rocket spacecraft, start balance, speed-raising is slow, process is long, spacecraft is subject to acceleration/accel impulsive force little.
3, track takes off, and system is easily controlled, and place builds that cost is low, emission process less infringement orbiting motion platform and aircraft platform, all can repeated multiple timesly use, and polytypic is general.
4, the lift-off of aircraft platform carrying two-stage rocket spacecraft, can laterally cross at a distance, and transmitting site restriction is few, can select and chase launch window, and the effects limit such as climate, meteorology and impact are less.
Four, accompanying drawing explanation:
Accompanying drawing 1 completes the front part plan schematic diagram of the orbit accelerating airplane of two-stage rocket spacecraft lift-off for two-stage motion platform.
Accompanying drawing 2 completes the lateral plane schematic diagram of the orbit accelerating airplane of two-stage rocket spacecraft lift-off for two-stage motion platform.
Reference numeral: 1, the base of the rail; 2, track; 3, orbiting motion platform; 4, aircraft platform; 5, two-stage rocket spacecraft.
Five, the specific embodiment:
As shown in Figure 1 and Figure 2, to complete orbit accelerating airplane, its track 2 of two-stage rocket spacecraft lift-off be to originate in the reliable base of the rail 1 of having of composing room, the outward extending double track of ray shape to two-stage motion platform of the present invention.Its orbiting motion platform 3 be have autonomous active power system, by orbiting motion platform negative pressure disconnecting gear, fastening and carry aircraft platform 4, accelerate and discharge aircraft platform 4, along streamline contour, the high-performance express locomotive of track 2 operation.Its aircraft platform 4 is that top circular arc flute profile rocket dress open, fastening by aircraft platform negative pressure disconnecting gear and that carry two-stage rocket spacecraft is taken storehouse in conventional cabin Position Design, and the cockpit of aircraft platform 4 is arranged at fuselage head below, rudder fin is set to outer Zhang Shuanyi.
Except the technical characterictic described in specification sheets, be those skilled in the art oneself know technology.
Claims (6)
1. two-stage motion platform completes an orbit accelerating airplane for two-stage rocket spacecraft lift-off, and it comprises track, orbiting motion platform, aircraft platform and two-stage rocket spacecraft, is characterized in that by orbiting motion platform, aircraft platform, the interim relay campaign of two-stage rocket is transmitted operation spacecraft is sent into planned orbit, and the rocket dress that its two-stage rocket spacecraft integral body is anchored on aircraft platform by aircraft platform negative pressure disconnecting gear is taken in storehouse, aircraft platform is anchored on orbiting motion platform by orbiting motion platform negative pressure disconnecting gear, pack up alighting gear, orbiting motion platform accelerates fast linear running along track under self power system and the traction of aircraft platform jet engine dual dynamic, when its running velocity surmounts aircraft platform takeoff speed, orbiting motion platform negative pressure disconnecting gear is opened, let aircraft platform fly away and take off, aircraft platform dependence self jet engine power carries rocket dress and takes the two-stage rocket spacecraft acceleration flight in storehouse and climb, to in advection layer during ceiling altitude, select the optimum transmit window of two-stage rocket spacecraft, start the jet engine running of two-stage rocket spacecraft, when two-stage rocket spacecraft flight power surmounts aircraft platform flying speed, aircraft platform is aimed at the flight of the launch window elevation angle, and the differential force that two-stage rocket spacecraft and aircraft platform form is opened aircraft platform negative pressure disconnecting gear, let two-stage rocket spacecraft fly away, enter programmed remote control flight, aircraft platform is selected the conventional landing in suitable airport.
2. two-stage motion platform according to claim 1 completes the orbit accelerating airplane of two-stage rocket spacecraft lift-off, it is characterized in that its track is ray shape, double rail type, for orbiting motion platform, parks, moves, accelerates and be decelerated to dedicated track out of service.
3. two-stage motion platform according to claim 1 completes the orbit accelerating airplane of two-stage rocket spacecraft lift-off, it is characterized in that its orbiting motion platform is to have autonomous active power system, by orbiting motion platform negative pressure disconnecting gear, fastening and carry aircraft platform, acceleration and discharge aircraft platform, Orbiting streamline contour, high-power, express locomotive.
4. two-stage motion platform according to claim 1 completes the orbit accelerating airplane of two-stage rocket spacecraft lift-off, the conventional cabin Position Design that it is characterized in that its aircraft platform is that top is open, circular arc flute profile rocket dress fastening by aircraft platform negative pressure disconnecting gear and that carry two-stage rocket spacecraft is taken storehouse, aircraft platform cockpit is arranged at fuselage head below, rudder fin is set to outer Zhang Shuanyi, the special-shaped aircraft that the jet engine of take is power.
5. two-stage motion platform according to claim 1 completes the orbit accelerating airplane of two-stage rocket spacecraft lift-off, the alighting gear that it is characterized in that its aircraft platform is packed up after aircraft platform is anchored on orbiting motion platform, to the aerial mission overall process that completes aircraft platform, before landing, open and put, in conventional airfield runway landing.
6. two-stage motion platform according to claim 1 completes the orbit accelerating airplane of two-stage rocket spacecraft lift-off, it is characterized in that its aircraft platform as aerospace master carrying and let three grades, one-stage rocket spacecraft fly away, or other forms and function, the spacecraft of different orbits.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210024472.1A CN102556360B (en) | 2012-02-06 | 2012-02-06 | Orbit accelerating airplane capable of completing lift-off of two-stage rocket spacecraft with two-stage moving platforms |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210024472.1A CN102556360B (en) | 2012-02-06 | 2012-02-06 | Orbit accelerating airplane capable of completing lift-off of two-stage rocket spacecraft with two-stage moving platforms |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102556360A CN102556360A (en) | 2012-07-11 |
| CN102556360B true CN102556360B (en) | 2014-04-02 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201210024472.1A Expired - Fee Related CN102556360B (en) | 2012-02-06 | 2012-02-06 | Orbit accelerating airplane capable of completing lift-off of two-stage rocket spacecraft with two-stage moving platforms |
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Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105584640A (en) * | 2016-03-10 | 2016-05-18 | 上海洲跃生物科技有限公司 | Vertical takeoff device of carrier-based aircraft |
| CN107054680A (en) * | 2017-01-21 | 2017-08-18 | 秦赵修 | The low windage pipeline of simulation stratosphere of built-in tracks |
| CN107804472A (en) * | 2017-10-06 | 2018-03-16 | 廖忠民 | High-speed locomotive booster system |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0778808A1 (en) * | 1994-09-02 | 1997-06-18 | Kistler Aerospace Corporation | Methods and apparatus for reusable launch platform and reusable spacecraft |
| CN2506543Y (en) * | 2001-08-27 | 2002-08-21 | 杨效权 | Launching test stand for astronautic air vehicle |
| CN101348166A (en) * | 2008-09-11 | 2009-01-21 | 杨举 | Takeoff and landing method for aircraft carrier-based aircraft and apparatus thereof |
| CN202624648U (en) * | 2012-02-06 | 2012-12-26 | 董兰田 | Track acceleration plane using two stages of motion platforms to finish levitation of two-stage rocket spacecraft |
-
2012
- 2012-02-06 CN CN201210024472.1A patent/CN102556360B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0778808A1 (en) * | 1994-09-02 | 1997-06-18 | Kistler Aerospace Corporation | Methods and apparatus for reusable launch platform and reusable spacecraft |
| CN2506543Y (en) * | 2001-08-27 | 2002-08-21 | 杨效权 | Launching test stand for astronautic air vehicle |
| CN101348166A (en) * | 2008-09-11 | 2009-01-21 | 杨举 | Takeoff and landing method for aircraft carrier-based aircraft and apparatus thereof |
| CN202624648U (en) * | 2012-02-06 | 2012-12-26 | 董兰田 | Track acceleration plane using two stages of motion platforms to finish levitation of two-stage rocket spacecraft |
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| CN102556360A (en) | 2012-07-11 |
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