CN101975529A - High-altitude rocket launching system - Google Patents
High-altitude rocket launching system Download PDFInfo
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- CN101975529A CN101975529A CN2010102610691A CN201010261069A CN101975529A CN 101975529 A CN101975529 A CN 101975529A CN 2010102610691 A CN2010102610691 A CN 2010102610691A CN 201010261069 A CN201010261069 A CN 201010261069A CN 101975529 A CN101975529 A CN 101975529A
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Abstract
The invention relates to a high-altitude rocket launching system in the atmospheric layer. The high-altitude carrier rocket launching system can launch a carrier rocket at high altitude in the atmospheric layer or launch the rocket to an opponent by being closer to the three-dimensional space of the opponent. As the high-altitude rocket launching system can save the chemical energy pushing course, the high-altitude rocket launching system can save a large amount of chemical energy, greatly improve the carrying capacity of the rocket, further greatly improve the launching efficiency and greatly reduce the launching cost. Furthermore, the high-altitude rocket launching system can be recycled and launch the rocket in a streamline operation way. The high-altitude rocket launching system consists of an intelligent information system, an intelligent control giant balloon, a carrying balloon system, a ground carrying system, the carrier rocket, an attack rocket, an engine and energy system and a protection system.
Description
One, field under the present invention:
The present invention is a kind of endoatmosphere high altitude rocket emission system.
Two, background technology:
At present, existing ground carrier rocket launch cost is high, and is also very big to ground pollution, greatly limited on a large scale to the personnel of space and the delivery of goods and materials.
Three, content of the present invention:
The present invention can solve above technology and use defective.High-altitude of the present invention carrier rocket emission system can be carried out the carrier rocket emission in endoatmospheric high-altitude, or more close enemy's solid space is fired a rocket to the enemy.Because saved the distance that chemical energy promotes, so just both saved a large amount of chemical energy, also can greatly improve the carrying capacity of rocket, thereby can greatly improve emission effciency, also greatly reduce launch cost.And the energy cycling and reutilization is fired a rocket with flow system.
High-altitude of the present invention carrier rocket emission system is made of intelligent information system Based Intelligent Control large balloon system, delivery balloon system, ground delivery system, carrier rocket, attack rocket, engine and energy resource system, guard system.As shown in Figure 1.
1, the large balloon system is the location large balloon of balloon protective cover (seeing the relevant patent of my balloon protective cover for details).Can directly put down rocket from its outlet, treat that rocket drops to desired location after, igniting emission.As shown in Figure 2.
2, delivery balloon system makes or is combined into different shape according to purposes is different with environment: ring-type delivery balloon, box-shaped delivery balloon or spherical balloon etc.
1) ring-type delivery balloon is the shape of lifebuoy formula, is made of balloon circle, hawser, sucker hook system, engine and energy resource system.
Each balloon circle has main gasbag, a few circle ballonet, air valve, air exhauster, and every circle air bag is divided into littler air chamber again, and adjacent air chamber links to each other with air valve, and any one or several air chamber gas leakage can not influence other air chamber.As shown in Figure 3.
Ring-type delivery balloon is used for vertically mentioning the high-altitude from ground with rocket, during the uncommon thin appropriate location of the atmosphere before the delivery balloon will reach the highest atmosphere that it can stop, make rocket firing, rocket is with bigger initial velocity, reaching the nearest atmosphere height of corresponding astronautical speed, the attitude of ability to require, by the energy operation that carries, just can save a lot of energy, and can reduce atmosphere than the atmospheric pressure layer, harmful effect than strong wind during to the rocket high-speed flight, so as more accurately with correct speed and angle satellite, sky and space plane or other object are delivered to the correct position of space.As shown in Figure 2.
With the ring-type balloon-rocket combination is firmly balanced in order to guarantee to promote rocket, just can make balloon and rocket all remain correct attitude.The balloon system increases and decreases the number of balloon capsule gradually to increase and decrease the tractive force that buoyancy provides rocket to move up and down.
Its sucker system holds rocket, and towing rocket was up when balloon was risen by atmospheric buoyancy force.Wherein certain air bag keeps inflated condition to control the attitude of this balloon system.To reduce gradually the number of the inflation of air bag is controlled downstream rate when balloon is descending.Balloon is being carried by the operation thing when up, to increase the number of the inflation of ballonet is controlled speed uplink.With big as far as possible initial velocity, rocket starts, and flies to target.As shown in Figure 2.
Also can propose carrier rocket from the large balloon of location with the ring-type balloon, to setting the spatial domain, rocket starts, when rocket oneself can balance be held, keep certain hour, treat that sucker and hawser unclamp after, adding high thrust again will be sent into the target location worker by load, or target of attack.As shown in Figure 4.
Also can make rocket keep set angle, allow rocket drop, to set apart from balloon apart from the time, rocket starts, and flies to target.As shown in Figure 4.
2) box-shaped delivery balloon is that shape is as chest.Rocket places in it, after setting the spatial domain, puts down rocket, igniting emission when rocket drops to desired location in it.As shown in Figure 6.
3) ring-type delivery balloon, box-shaped delivery balloon and spherical delivery balloon can fly out to go to and set the spatial domain and fire a rocket from the large balloon system.As shown in Figure 7 and Figure 8.
Four, description of drawings:
Fig. 1 is the structure chart of high-altitude carrier rocket emission system;
Fig. 2 is the schematic diagram that the large balloon system directly fires a rocket:
1. locate large balloon 2. rocket 3. import and export
Fig. 3 is the schematic diagram of ring-type delivery balloon Vertical Launch rocket:
1. 2. ring-type delivery balloon of rocket
Fig. 4 is the structure chart of ring-type delivery balloon:
Fig. 5 is the schematic diagram that ring-type delivery balloon inclined is fired a rocket:
1. 2. ring-type delivery balloon of rocket
Fig. 6 is a box-shaped delivery balloon borne rocket schematic diagram:
1. 2. box-shaped delivery balloon of rocket
Fig. 7 is that box-shaped delivers balloon from locating the schematic diagram of firing a rocket behind the large balloon end opening:
1. locate large balloon 2. rocket 3. box-shaped delivery balloon 4. import and export
Fig. 8 box-shaped delivery balloon is from locating the schematic diagram of firing a rocket behind the large balloon end opening:
1. locate large balloon and 2. import and export 3. 4. rocket of box-shaped delivery balloon
Fig. 9 ring-type delivery balloon is from locating the schematic diagram of firing a rocket behind the large balloon:
1. locate large balloon and 2. import and export 3. 4. rocket of ring-type delivery balloon
Claims (8)
1. the present invention is a kind of endoatmosphere high altitude rocket emission system.
2. according to right 1 described a kind of endoatmosphere high altitude rocket emission system, it is characterized in that: can carry out the carrier rocket emission in endoatmospheric high-altitude, or more close enemy's solid space is fired a rocket to the enemy.Because saved the distance that chemical energy promotes, so just both saved a large amount of chemical energy, also can greatly improve the carrying capacity of rocket, thereby can greatly improve emission effciency, also greatly reduce launch cost.And the energy cycling and reutilization is fired a rocket with flow system.
3. according to right 1 described a kind of endoatmosphere high altitude rocket emission system, it is characterized in that: constitute by intelligent information system Based Intelligent Control large balloon system, delivery balloon system, ground delivery system, carrier rocket, attack rocket, engine and energy resource system, guard system.
4. according to the described delivery balloon of right 3 system, it is characterized in that: ring-type delivery balloon, box-shaped delivery balloon or spherical balloon etc.
5. according to right 4 described a kind of ring-type delivery balloons, it is characterized in that: be the shape of lifebuoy formula, constitute by balloon circle, hawser, sucker hook system, engine and energy resource system.Each balloon circle has main gasbag, a few circle ballonet, air valve, air exhauster, and every circle air bag is divided into littler air chamber again, and adjacent air chamber links to each other with air valve, and any one or several air chamber gas leakage can not influence other air chamber.
Ring-type delivery balloon is used for vertically mentioning the high-altitude from ground with rocket, during the uncommon thin appropriate location of the atmosphere before the delivery balloon will reach the highest atmosphere that it can stop, make rocket firing, rocket is with bigger initial velocity, reaching the nearest atmosphere height of corresponding astronautical speed, the attitude of ability to require, by the energy operation that carries, just can save a lot of energy, and can reduce atmosphere than the atmospheric pressure layer, harmful effect than strong wind during to the rocket high-speed flight, so as more accurately with correct speed and angle satellite, sky and space plane or other object are delivered to the correct position of space.
With the ring-type balloon-rocket combination is firmly balanced in order to guarantee to promote rocket, just can make balloon and rocket all remain correct attitude.The balloon system increases and decreases the number of balloon capsule gradually to increase and decrease the tractive force that buoyancy provides rocket to move up and down.
Its sucker system holds rocket, and towing rocket was up when balloon was risen by atmospheric buoyancy force.Wherein certain air bag keeps inflated condition to control the attitude of this balloon system.To reduce gradually the number of the inflation of air bag is controlled downstream rate when balloon is descending.Balloon is being carried by the operation thing when up, to increase the number of the inflation of ballonet is controlled speed uplink.With big as far as possible initial velocity, rocket starts, and flies to target.As shown in Figure 2.
Also can propose carrier rocket from the large balloon of location with the ring-type balloon, to setting the spatial domain, rocket starts, when rocket oneself can balance be held, keep certain hour, treat that sucker and hawser unclamp after, adding high thrust again will be sent into the target location worker by load, or target of attack.As shown in Figure 4.
Also can make rocket keep set angle, allow rocket drop, to set apart from balloon apart from the time, rocket starts, and flies to target.
6. box-shaped delivery balloon is that shape is as chest.Rocket places in it, after setting the spatial domain, puts down rocket, igniting emission when rocket drops to desired location in it.
7. maintenance system, make-up system, survival system and transfer system are aerial personnel and goods and materials service at ordinary times.
8. ring-type delivery balloon, box-shaped delivery balloon and spherical delivery balloon can fly out from the large balloon system, fire a rocket to setting the spatial domain again.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102610691A CN101975529A (en) | 2010-08-24 | 2010-08-24 | High-altitude rocket launching system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102610691A CN101975529A (en) | 2010-08-24 | 2010-08-24 | High-altitude rocket launching system |
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| Publication Number | Publication Date |
|---|---|
| CN101975529A true CN101975529A (en) | 2011-02-16 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010102610691A Pending CN101975529A (en) | 2010-08-24 | 2010-08-24 | High-altitude rocket launching system |
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| CN (1) | CN101975529A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105819002A (en) * | 2016-04-08 | 2016-08-03 | 湖北航天技术研究院总体设计所 | Near space satellite launching platform and method |
| CN106628251A (en) * | 2016-12-19 | 2017-05-10 | 范子盛 | Combined spacecraft and orbiter launching and recycling method |
| CN107804481A (en) * | 2017-10-06 | 2018-03-16 | 廖忠民 | Dirigible assist system |
-
2010
- 2010-08-24 CN CN2010102610691A patent/CN101975529A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105819002A (en) * | 2016-04-08 | 2016-08-03 | 湖北航天技术研究院总体设计所 | Near space satellite launching platform and method |
| CN106628251A (en) * | 2016-12-19 | 2017-05-10 | 范子盛 | Combined spacecraft and orbiter launching and recycling method |
| CN107804481A (en) * | 2017-10-06 | 2018-03-16 | 廖忠民 | Dirigible assist system |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110216 |