CN106965955A - A kind of recoverable reusable carrier rocket of parachuting - Google Patents
A kind of recoverable reusable carrier rocket of parachuting Download PDFInfo
- Publication number
- CN106965955A CN106965955A CN201710147767.0A CN201710147767A CN106965955A CN 106965955 A CN106965955 A CN 106965955A CN 201710147767 A CN201710147767 A CN 201710147767A CN 106965955 A CN106965955 A CN 106965955A
- Authority
- CN
- China
- Prior art keywords
- recoverable
- parachuting
- carrier rocket
- rocket
- return
- 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
- 230000000694 effects Effects 0.000 abstract description 2
- 239000003380 propellant Substances 0.000 abstract 1
- 239000002699 waste material Substances 0.000 abstract 1
- 230000007423 decrease Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 1
- 239000012050 conventional carrier Substances 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The present invention is a kind of recoverable reusable carrier rocket of parachuting, is divided into overall recoverable configuration and the recoverable class of configuration two of split.Using the recoverable carrier rocket of parachuting mode, the effect of reuse can be reached, while reducing the propellant waste in return course, landing reliability and security is improved.Split type return parachuting configuration can also carry out return control, including landing point, landing speed, posture etc. to rocket section respectively according to demand.
Description
Technical field
The invention is under the jurisdiction of space launch vehicle technology field.
Background technology
The background of invention technology includes carrier rocket technology, reusable carrier rocket technology, parachuting technology.
The content of the invention
The present invention proposes a kind of parachuting formula reusing carrier rocket.Utilization and recycle carrier rocket, is especially reclaimed multiple
Use the first order（Also referred to as base level）Carrier rocket or rocket booster have high economic value, can reduce carrier rocket
Single emission cost, improves profit margin.
The recoverable reusable carrier rocket of parachuting is the carrier rocket that ground is returned to by parachute ways of deceleration, Ke Yiduo
It is secondary to reuse.After being separated with upper level carrier rocket or load, the recoverable carrier rocket of parachuting is subtracted by releasing a parachute
Speed, carrier rocket posture is adjusted by attitude control motor, and the effect slowed down according to parachute may be selected when close to ground
Push away engine using counter and further slow down, do contact buffering with ground using the support that rises and falls, coordinate gesture stability to deliver fire
Arrow is stable to be parked in landing field on the ground.The general subsystem of the type rocket, including dynamical system, control system, gesture stability
System etc. is identical with conventional carrier rocket.
It is different with the form of return according to the position for installing parachute, or according to different return demands, parachuting is recoverable
Reusable carrier rocket is divided into overall recoverable（Echo plex mode is shown in Fig. 1）It is recoverable with split（Echo plex mode is shown in Fig. 2）Two kinds.
（1）Overall recoverable reusing carrier rocket
The configuration carrier rocket is begun to decline by integral form from reentry point, keeps overall structure constant during decline,
Until overall landing.This process schematic that lands is shown in Fig. 1.
（2）The recoverable reusing carrier rocket of split
The recoverable reusing carrier rocket of split configuration is begun to decline from reentry point, is resolved into during decline different
Rocket body part, abandons the part that need not be returned, it is necessary to which each Self-opened umbrella landing is distinguished in the part returned as needed.Descent
Schematic diagram is shown in Fig. 2.This mode is more suitable for the heavier heavy launcher of rocket body structure.
Brief description of the drawings
Fig. 1 is the recoverable reusable carrier rocket return course schematic diagram of overall configuration parachuting；
Fig. 2 is the recoverable reusable carrier rocket return course schematic diagram of split configuration parachuting.
Claims (3)
1. require to carry out protection of the patent right to the recoverable reusable carrier rocket of parachuting, it is adaptable to the return of arbitrary form parachute
Formula carrier rocket.
2. return to pattern for split, it is desirable to only carrying out certain mode（Such as retro-rocket formula）Split return, but do not make
Protection of the patent right is carried out with the situation of parachute.
3. require to carry out protection of the patent right to the application mode of this rocket of recoverable reurnable booster.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710147767.0A CN106965955A (en) | 2017-03-14 | 2017-03-14 | A kind of recoverable reusable carrier rocket of parachuting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710147767.0A CN106965955A (en) | 2017-03-14 | 2017-03-14 | A kind of recoverable reusable carrier rocket of parachuting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106965955A true CN106965955A (en) | 2017-07-21 |
Family
ID=59329452
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710147767.0A Pending CN106965955A (en) | 2017-03-14 | 2017-03-14 | A kind of recoverable reusable carrier rocket of parachuting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106965955A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110095032A (en) * | 2019-05-28 | 2019-08-06 | 蓝箭航天空间科技股份有限公司 | A kind of liquid rocket recovery method |
| CN110108171A (en) * | 2019-05-28 | 2019-08-09 | 蓝箭航天空间科技股份有限公司 | A kind of liquid rocket |
| CN110588977A (en) * | 2019-09-25 | 2019-12-20 | 北京凌空天行科技有限责任公司 | Solid rocket aircraft |
| CN110779399A (en) * | 2019-10-23 | 2020-02-11 | 北京空间机电研究所 | Metal honeycomb buffering-based one-stage rocket body hanging conversion device and method for carrier rocket |
| CN112146525A (en) * | 2020-09-03 | 2020-12-29 | 北京星际荣耀空间科技有限公司 | Carrier rocket upper-level recovery method and recovery system |
| CN115848624A (en) * | 2023-02-24 | 2023-03-28 | 北京瀚科智翔科技发展有限公司 | Hanging type aviation containerized carrier for umbrella-free air drop |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1421673A (en) * | 2001-11-30 | 2003-06-04 | 联合工艺公司 | Repeatable using space entry carrier rocket system |
| CN105398583A (en) * | 2009-06-15 | 2016-03-16 | 蓝源有限责任公司 | Sea Landing Of Space Launch Vehicles And Associated Systems And Methods |
| US20160280399A1 (en) * | 2013-11-27 | 2016-09-29 | Vladimir Vladimirovich Tkach | Rocket engine recovery system |
| CN106021628A (en) * | 2015-07-03 | 2016-10-12 | 中国运载火箭技术研究院 | Vertical returning trajectory design method for carrier rocket |
-
2017
- 2017-03-14 CN CN201710147767.0A patent/CN106965955A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1421673A (en) * | 2001-11-30 | 2003-06-04 | 联合工艺公司 | Repeatable using space entry carrier rocket system |
| CN105398583A (en) * | 2009-06-15 | 2016-03-16 | 蓝源有限责任公司 | Sea Landing Of Space Launch Vehicles And Associated Systems And Methods |
| US20160280399A1 (en) * | 2013-11-27 | 2016-09-29 | Vladimir Vladimirovich Tkach | Rocket engine recovery system |
| CN106021628A (en) * | 2015-07-03 | 2016-10-12 | 中国运载火箭技术研究院 | Vertical returning trajectory design method for carrier rocket |
Non-Patent Citations (2)
| Title |
|---|
| 汪小卫;张普卓;吴胜宝;申麟;: "运载火箭子级回收技术研究" * |
| 高朝辉;张普卓;刘宇;余梦伦;: "垂直返回重复使用运载火箭技术分析" * |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110095032A (en) * | 2019-05-28 | 2019-08-06 | 蓝箭航天空间科技股份有限公司 | A kind of liquid rocket recovery method |
| CN110108171A (en) * | 2019-05-28 | 2019-08-09 | 蓝箭航天空间科技股份有限公司 | A kind of liquid rocket |
| CN110095032B (en) * | 2019-05-28 | 2020-11-06 | 蓝箭航天空间科技股份有限公司 | Liquid rocket recovery method |
| CN110108171B (en) * | 2019-05-28 | 2024-05-07 | 蓝箭航天空间科技股份有限公司 | Liquid rocket |
| CN110588977A (en) * | 2019-09-25 | 2019-12-20 | 北京凌空天行科技有限责任公司 | Solid rocket aircraft |
| CN110588977B (en) * | 2019-09-25 | 2021-03-23 | 北京凌空天行科技有限责任公司 | Solid rocket aircraft |
| CN110779399A (en) * | 2019-10-23 | 2020-02-11 | 北京空间机电研究所 | Metal honeycomb buffering-based one-stage rocket body hanging conversion device and method for carrier rocket |
| CN112146525A (en) * | 2020-09-03 | 2020-12-29 | 北京星际荣耀空间科技有限公司 | Carrier rocket upper-level recovery method and recovery system |
| CN115848624A (en) * | 2023-02-24 | 2023-03-28 | 北京瀚科智翔科技发展有限公司 | Hanging type aviation containerized carrier for umbrella-free air drop |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170721 |
|
| WD01 | Invention patent application deemed withdrawn after publication |