CN1136523A - Runway taking-off, air-launching space shuttle - Google Patents
Runway taking-off, air-launching space shuttle Download PDFInfo
- Publication number
- CN1136523A CN1136523A CN 95118902 CN95118902A CN1136523A CN 1136523 A CN1136523 A CN 1136523A CN 95118902 CN95118902 CN 95118902 CN 95118902 A CN95118902 A CN 95118902A CN 1136523 A CN1136523 A CN 1136523A
- Authority
- CN
- China
- Prior art keywords
- space shuttle
- engine
- air
- space
- runway
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Abstract
The problems to be solved is the trial and error, design and hanging of the hanging type jet-engine, the operational quality of space shuttle and the improvement of the wing. The main technological characteristics are that the space shuttle utilizes the thrust of hanging type jet-engine under the wing and the lift produced by the wing to take-off on the runway of the airport, under a specific height and speed condition the hanging type jet-engine is shut off and abanded, then the engine of the rocket is ignited and launched from the space to the orbit of the earth. It is used for entering cosmic space freely under the conditions of safety, ease and low cost.
Description
The invention belongs to aeronautical and space technology space shuttle lift-off technology field.
The present general vertical launch mode of employing of the United States, Russia's space shuttle institute.
The high thrust performance of jet engine now.(Boeing-747 is born the space shuttle ferry flight)
(secondary in the multi-stage rocket emission process and the igniting of three-stage rocket flight) is launched in in-flight ingition again.
Annotate: above-described technological document very easily is found, and is common people and knows!
Provide a kind of convenience, safety and comparatively popular space shuttle launching technique to open up road for the human freedom enters the sky, universe.
Runway takes off, launches the space shuttle technical description in the air:
Realize that this kind mode launches space shuttle and must at first realize 2 points: 1, the conventional jet engine device of suspension type; 2, space shuttle some transformations that should carry out.
1, the general structure of the conventional jet engine device of suspension type and hang the position: rationally match according to emission rank (being size, the weight of space shuttle), adopt suitable jet engine, its driving engine, fuel tank, suspension bracket adopt integrated structure design, whole device is hung under the wing by the point of the conformal carriage under the space shuttle wing, and form thus that runway takes off, the power of airflight, the profile of whole device and structure determine specifically that according to actual conditions driving engine is preferably selected the engine of Boeing-747 for use.
2, space shuttle some transformations that should carry out: set store mounting point and desertion device and the wing profile of therefore carrying out and the reinforcement of inner structure thereof under (1) wing; (2) improvement of the handling quality of space shuttle; (3) rocket cowling and desertion device thereof in the aerodynamic flight process; (4) external hanging fuel of space shuttle rocket and booster rocket are that integral type is hung under the aircraft ventral.
Runway takes off, launches the roughly process of space shuttle in the air: 1, the space shuttle of the good conventional jet engine device of lifting is carried out and is taken off and launch; 2, space shuttle utilizes jet engine to carry out runway to take off; 3, space shuttle carries out course and attitude adjustment after rising to certain altitude; 4, throw rocket engine afterbody fairing down, rocket engine and booster rocket are prepared igniting.5, close jet engine and abandoning; 6, space shuttle sustainer rocket engine and booster rocket igniting emission; 7, space shuttle carries out last attitude adjustment, the preparation injection; 8, booster rocket and plug-in fuel are used up, and abandon the space shuttle injection; 9, reclaim various discards.
If abnormal condition (as rocket motor ignition failure, phenomenons such as engine breakdown) appear in space shuttle in emission process, space shuttle can interrupt emission fully, adopts the gliding flight mode in the safe landing of Adequate Aerodrome runway.Beneficial effect: (1) shortens the space shuttle launch preparation time, improves emission efficiency;
(2) reduce the space shuttle launch cost, simplify launch facility;
(3) improve the safety that space shuttle is launched;
Claims (1)
- The present invention relates to the launch mode that a kind of runway takes off, launches space shuttle in the air.Its common characteristic is: aloft (under certain altitude and the certain flying speed) carries out secondary emission.Inventive features: its domestic animal is to utilize the conventional jet engine device of suspension type that space shuttle is taken off from airfield runway, and under the situation of certain altitude, speed, abandon the conventional jet engine device of suspension type, utilize space shuttle rocket engine and suspension type booster rocket from space shuttle being launched into Earth's orbit in the air.To the launch mode in the invention and for realize conventional jet engine device of suspension type that this launch mode carries out and space shuttle some transformations that should carry out protection is provided.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 95118902 CN1136523A (en) | 1995-11-02 | 1995-11-02 | Runway taking-off, air-launching space shuttle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 95118902 CN1136523A (en) | 1995-11-02 | 1995-11-02 | Runway taking-off, air-launching space shuttle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1136523A true CN1136523A (en) | 1996-11-27 |
Family
ID=5081801
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 95118902 Pending CN1136523A (en) | 1995-11-02 | 1995-11-02 | Runway taking-off, air-launching space shuttle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1136523A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105026262A (en) * | 2012-12-20 | 2015-11-04 | 空中客车防卫和太空有限责任公司 | Auxiliary device for high-flying aircraft |
-
1995
- 1995-11-02 CN CN 95118902 patent/CN1136523A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105026262A (en) * | 2012-12-20 | 2015-11-04 | 空中客车防卫和太空有限责任公司 | Auxiliary device for high-flying aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4802639A (en) | Horizontal-takeoff transatmospheric launch system | |
| US4265416A (en) | Orbiter/launch system | |
| CA1330071C (en) | Rocket-powered, air-deployed, lift-assisted booster vehicle for orbital, supraorbital and suborbital flight | |
| RU2191145C2 (en) | System of injection of payload into low-altitude near-earth orbit | |
| US8528853B2 (en) | In-line staged horizontal takeoff and landing space plane | |
| CN110589034B (en) | Recyclable high-speed flying rocket and recycling method | |
| RU2000114837A (en) | SYSTEM FOR TRANSFORMING A SELF-SUPPORTED HORIZONTAL FLIGHT PLANE AND A HORIZONTAL TAKE-OFF IN A HYBRID COMBINED SELF-SUPPORTED HORIZONTAL FLIGHT AROUND | |
| JPH10509113A (en) | A space launch aircraft configured like a glider and towed by conventional aircraft to increase altitude | |
| GB2222635A (en) | A propulsion system for an aerospace vehicle | |
| CN109764774A (en) | A kind of experimental rig returning to landing mission for simulated rocket | |
| US20040031880A1 (en) | Aircraft and propulsion system for an aircraft, and operating method | |
| CN102730179A (en) | Combined lifting force deformation airship | |
| CN101954973A (en) | Helicopter, weapon and equipment capable of realizing zero/zero ejection | |
| JP4632112B2 (en) | Satellite launch method | |
| CN109850142A (en) | Novel jet can vertical translation aircraft and new aeropropulsion system | |
| CN1136523A (en) | Runway taking-off, air-launching space shuttle | |
| CN113232854B (en) | Distributed unmanned aerial vehicle platform applied to ballistic launching and launching method | |
| US20190193873A1 (en) | High Altitude Air Launched Rocket | |
| RU2715816C1 (en) | Accelerating carrier aircraft (versions) | |
| RU2061630C1 (en) | Interorbital aerospace vehicle | |
| CN103832582A (en) | Multifunctional helicopter | |
| RU2211784C2 (en) | Recoverable boost vehicle | |
| CN215285312U (en) | Air-based transmitting system based on double-body flat wing layout aircraft carrier | |
| Buttler | Jet Prototypes of World War II: Gloster, Heinkel, and Caproni Campini's Wartime Jet Programmes | |
| CN2313852Y (en) | Float for aircraft crash |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C01 | Deemed withdrawal of patent application (patent law 1993) | ||
| WD01 | Invention patent application deemed withdrawn after publication |