CN102556360A - 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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- CN102556360A CN102556360A CN2012100244721A CN201210024472A CN102556360A CN 102556360 A CN102556360 A CN 102556360A CN 2012100244721 A CN2012100244721 A CN 2012100244721A CN 201210024472 A CN201210024472 A CN 201210024472A CN 102556360 A CN102556360 A CN 102556360A
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- 230000001133 acceleration Effects 0.000 claims abstract description 9
- 238000000034 method Methods 0.000 claims description 4
- 230000009977 dual effect Effects 0.000 claims description 3
- 230000003137 locomotive effect Effects 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims description 2
- 239000005437 stratosphere Substances 0.000 abstract 2
- 239000000446 fuel Substances 0.000 abstract 1
- 239000005436 troposphere Substances 0.000 abstract 1
- JJWKPURADFRFRB-UHFFFAOYSA-N carbonyl sulfide Chemical compound O=C=S JJWKPURADFRFRB-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
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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 track acceleration aircraft that a kind of two-stage motion platform is accomplished the lift-off of two-stage rocket spacecraft.
Two, background technology:
The three-stage rocket relay boosting spacecraft that father's Tsiolkovsky of space flight is founded gets into the theory of space; Become design, the design of existing space technology, the basic model of practice; But; Extension and expansion along with the mankind explore and utilize the cosmic space to transmitting frequency, scale, the distance of going deep into space and return etc., are all producing the comprehensive demand that matter, amount, technical risk and cost reduce.Prior art is faced with the rocket volume and the boosting power limit, launch site addressing, weather, meteorological follow, the restriction of numerous aspects such as accurate assurance of launch window.
Three, summary of the invention:
The objective of the invention is limitation, provide a kind of cost track that two-stage motion platform low, reusable, that can select and chase launch window is accomplished the lift-off of two-stage rocket spacecraft to quicken aircraft to above demand and prior art.
The objective of the invention is to realize through following technical scheme:
The track that a kind of two-stage motion platform is accomplished the lift-off of two-stage rocket spacecraft quickens aircraft; It comprises track, orbiting motion platform, aircraft platform and two-stage rocket spacecraft; It is characterized in that spacecraft being sent into planned orbit through the interim relay Motion Transmission operation of orbiting motion platform, aircraft platform, two-stage rocket; Its two-stage rocket spacecraft integral body through the rocket dress that airplane motion platform negative pressure disconnecting gear is anchored on aircraft platform take in the storehouse, aircraft platform is anchored on the orbiting motion platform, packs up alighting gear through orbiting motion platform negative pressure disconnecting gear; The orbiting motion platform quickens linear running fast in self power system and aircraft platform jet engine dual dynamic traction lower edge track; When its running velocity is got over the aircraft platform takeoff speed, orbiting motion platform negative pressure disconnecting gear opens, let aircraft platform fly away takes off; Aircraft platform rely on self jet engine power carry the rocket dress take the two-stage rocket spacecraft storehouse in quicken flight and climb, to advection layer during ceiling altitude, select the two-stage rocket spacecraft the optimum transmit window, start the jet engine running of two-stage rocket spacecraft, when two-stage rocket spacecraft flight power surmounts the aircraft platform flying speed, aircraft platform aims at the launch window elevation angle and flies; The differential force that two-stage rocket spacecraft and aircraft platform form is opened aircraft platform negative pressure disconnecting gear, lets the two-stage rocket spacecraft fly away, is got into programmed remote control flight, and aircraft platform is selected the conventional landing in suitable airport.
Above-described track is ray shape, double rail type, the acceleration of confession orbiting motion platform, is decelerated to dedicated track out of service.
Described orbiting motion platform is to have autonomous active power system, through 3 orbiting motion platforms of preceding triangle negative pressure disconnecting gear, 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 through aircraft platform negative pressure disconnecting gear and carrying two-stage rocket spacecraft is taken the storehouse; The aircraft platform cockpit is arranged at the fuselage head below; Rudder fin is set to outer Zhang Shuanyi, is the special-shaped aircraft of power with the jet engine.
The alighting gear of described aircraft platform is promptly packed up after aircraft platform is anchored on the orbiting motion platform, to the aerial mission overall process of accomplishing aircraft platform, before landing, opens and puts, in conventional airfield runway landing.
Described aircraft platform can be used as aerospace master, carries and let fly away three grades, one-stage rocket spacecraft, other forms and spacecrafts function, different orbits.
The track that two-stage motion platform of the present invention is accomplished the lift-off of two-stage rocket spacecraft quickens aircraft compared with prior art, has following outstanding advantage:
1, the dual dynamic source with the aircraft platform of orbiting motion platform with powerful autonomous dynamic and jet engine power promotes to take off and accomplish and pass through convective zone and part advection layer; Let the booster-missile combination spacecraft fly away in the advection layer that minimum and terrestrial gravitation reduces at air resistance; The first order that replaces traditional three-stage rocket that power consumption is maximum, volume is maximum, risk is maximum makes that the spacecraft emission is safer, environmental protection, cost be lower.
2, carry emission two-stage rocket spacecraft by the two-stage motion platform, start balance, speed-raising is slow, process is long, spacecraft receives the acceleration/accel impulsive force little.
3, track takes off, and system is prone to control, and the place builds that cost is low, emission process less infringement orbiting motion platform and aircraft platform, but all repeated multiple times is used, and polytypic is general.
4, aircraft platform carries the lift-off of two-stage rocket spacecraft, traverse at a distance, and launch window selected and chased to the transmitting site restriction can less, receives effects limit such as weather, meteorology and influence less.
Four, description of drawings:
Accompanying drawing 1 is accomplished the front part plan scheme drawing of the track acceleration aircraft of two-stage rocket spacecraft lift-off for the two-stage motion platform.
Accompanying drawing 2 is accomplished the lateral plane scheme drawing of the track acceleration aircraft of two-stage rocket spacecraft lift-off for the 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:
Like Fig. 1, shown in Figure 2, the track that two-stage motion platform of the present invention is accomplished the lift-off of two-stage rocket spacecraft quickens aircraft, its track 2 is to originate in the reliable base of the rail 1 of having of composing room, the outward extending double track of ray shape.Its orbiting motion platform 3 be have autonomous active power system, through orbiting motion platform negative pressure disconnecting gear, fastening and carry aircraft platform 4, quicken and discharge aircraft platform 4, along streamline contour, the high-performance express locomotive of track 2 operations.Its aircraft platform 4 is that top circular arc flute profile rocket dress open, fastening through aircraft platform negative pressure disconnecting gear and carrying two-stage rocket spacecraft is taken the storehouse in conventional cabin Position Design, and the cockpit of aircraft platform 4 is arranged at the fuselage head below, rudder fin is set to outer Zhang Shuanyi.
Except that the described technical characterictic of specification sheets, oneself knowledge that is those skilled in the art is technological.
Claims (6)
1. a two-stage motion platform is accomplished the track acceleration aircraft that the two-stage rocket spacecraft goes up to the air; It comprises track, orbiting motion platform, aircraft platform and two-stage rocket spacecraft; It is characterized in that spacecraft being sent into planned orbit through the interim relay Motion Transmission operation of orbiting motion platform, aircraft platform, two-stage rocket; Its two-stage rocket spacecraft integral body through the rocket dress that airplane motion platform negative pressure disconnecting gear is anchored on aircraft platform take in the storehouse, aircraft platform is anchored on the orbiting motion platform, packs up alighting gear through orbiting motion platform negative pressure disconnecting gear; The orbiting motion platform quickens linear running fast in self power system and aircraft platform jet engine dual dynamic traction lower edge track; When its running velocity is got over the aircraft platform takeoff speed, orbiting motion platform negative pressure disconnecting gear opens, let aircraft platform fly away takes off; Aircraft platform rely on self jet engine power carry the rocket dress take the two-stage rocket spacecraft storehouse in quicken flight and climb, to advection layer during ceiling altitude, select the two-stage rocket spacecraft the optimum transmit window, start the jet engine running of two-stage rocket spacecraft, when two-stage rocket spacecraft flight power surmounts the aircraft platform flying speed, aircraft platform aims at the launch window elevation angle and flies; The differential force that two-stage rocket spacecraft and aircraft platform form is opened aircraft platform negative pressure disconnecting gear, lets the two-stage rocket spacecraft fly away, is got into programmed remote control flight, and aircraft platform is selected the conventional landing in suitable airport.
2. the track that two-stage motion platform according to claim 1 is accomplished the lift-off of two-stage rocket spacecraft quickens aircraft, it is characterized in that its track is that dedicated track out of service is parked, moves, quickens and be decelerated to ray shape, double rail type, confession orbiting motion platform.
3. the track that two-stage motion platform according to claim 1 is accomplished the lift-off of two-stage rocket spacecraft quickens aircraft; It is characterized in that its orbiting motion platform is to have autonomous active power system; Through 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. the track that two-stage motion platform according to claim 1 is accomplished the lift-off of two-stage rocket spacecraft quickens aircraft; 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 through aircraft platform negative pressure disconnecting gear and carrying two-stage rocket spacecraft is taken the storehouse; The aircraft platform cockpit is arranged at the fuselage head below, and rudder fin is set to outer Zhang Shuanyi, is the special-shaped aircraft of power with the jet engine.
5. the track that two-stage motion platform according to claim 1 is accomplished the lift-off of two-stage rocket spacecraft quickens aircraft; The alighting gear that it is characterized in that its aircraft platform is promptly packed up after aircraft platform is anchored on the orbiting motion platform; To the aerial mission overall process of accomplishing aircraft platform; Before landing, open and put, in conventional airfield runway landing.
6. the track that two-stage motion platform according to claim 1 is accomplished the lift-off of two-stage rocket spacecraft quickens aircraft; It is characterized in that its aircraft platform can be used as aerospace master and carries and let fly away three grades, one-stage rocket spacecraft; 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 true CN102556360A (en) | 2012-07-11 |
| CN102556360B CN102556360B (en) | 2014-04-02 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| 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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| CN (1) | CN102556360B (en) |
Cited By (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 |
| CN107804472A (en) * | 2017-10-06 | 2018-03-16 | 廖忠民 | Express locomotive assist system |
| WO2018133640A1 (en) * | 2017-01-21 | 2018-07-26 | 秦赵修 | Low-wind-resistance tubular track, stratosphere-simulating low-wind-resistance tube having built-in track, carrier rocket spacecraft launching system, and method for reducing resistance of tubular track |
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 |
Cited By (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 |
| WO2018133640A1 (en) * | 2017-01-21 | 2018-07-26 | 秦赵修 | Low-wind-resistance tubular track, stratosphere-simulating low-wind-resistance tube having built-in track, carrier rocket spacecraft launching system, and method for reducing resistance of tubular track |
| CN107804472A (en) * | 2017-10-06 | 2018-03-16 | 廖忠民 | Express locomotive assist system |
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| Publication number | Publication date |
|---|---|
| CN102556360B (en) | 2014-04-02 |
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Effective date of registration: 20190117 Address after: 223800 Shuangzhuang Auto Parts City A11-2, Suqian City, Jiangsu Province Patentee after: Jiangsu Junzhi Construction Co., Ltd. Address before: 250013 Room 301, Unit 4, Building 8, Luhe District, Lixia District, Jinan City, Shandong Province Patentee before: Dong Lantian |
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