GB0203513D0 - Satellite ejection mechanism - Google Patents
Satellite ejection mechanismInfo
- Publication number
- GB0203513D0 GB0203513D0 GBGB0203513.7A GB0203513A GB0203513D0 GB 0203513 D0 GB0203513 D0 GB 0203513D0 GB 0203513 A GB0203513 A GB 0203513A GB 0203513 D0 GB0203513 D0 GB 0203513D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- ejection mechanism
- satellite
- satellite ejection
- ejection
- 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.)
- Withdrawn
Links
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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
- B64G1/6457—Springs; Shape memory actuators
-
- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/641—Interstage or payload connectors
- B64G1/642—Clamps, e.g. Marman clamps
-
- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
- B64G1/6455—Pyrotechnics; Using heat
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
-
- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
- B64G1/6459—Fluid-actuated
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Actuator (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0203513A GB2385310A (en) | 2002-02-14 | 2002-02-14 | Satellite launch assembly including means for connection and release |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0203513A GB2385310A (en) | 2002-02-14 | 2002-02-14 | Satellite launch assembly including means for connection and release |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0203513D0 true GB0203513D0 (en) | 2002-04-03 |
GB2385310A GB2385310A (en) | 2003-08-20 |
Family
ID=9931078
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0203513A Withdrawn GB2385310A (en) | 2002-02-14 | 2002-02-14 | Satellite launch assembly including means for connection and release |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2385310A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109625339A (en) * | 2018-12-29 | 2019-04-16 | 西北工业大学 | A kind of micro-nano satellite separator of controllable rotating angular speed |
CN115009549A (en) * | 2022-08-09 | 2022-09-06 | 北京星河动力装备科技有限公司 | Locking and releasing mechanism, control method thereof and carrier rocket |
CN115057012A (en) * | 2022-08-03 | 2022-09-16 | 北京劢亚科技有限公司 | Multi-satellite chain type launching, locking, unlocking and ejecting mechanism |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2500591C1 (en) * | 2012-07-11 | 2013-12-10 | Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Aircraft compartment separation system |
RU2551181C2 (en) * | 2013-09-17 | 2015-05-20 | Закрытое акционерное общество "РК СТАРТ" | Method for obtaining additional pulse of missile thrust, and inter-stage accelerator for its implementation (versions) |
CN104071357B (en) * | 2014-07-08 | 2016-04-27 | 上海新跃仪表厂 | A kind of Technique in Rendezvous and Docking device |
CN105253327B (en) * | 2015-11-19 | 2017-03-22 | 浙江理工大学 | Centralized variable angle unfolding locking mechanism |
CN106628271B (en) * | 2016-11-09 | 2019-10-18 | 上海宇航系统工程研究所 | A kind of small miniature double revolving cup docking mechanisms |
CN111284731B (en) | 2020-01-16 | 2020-11-10 | 清华大学 | Electromagnetic locking and releasing mechanism for separating star from arrow and electromagnetic locking and releasing method |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2002307B (en) * | 1977-08-03 | 1982-01-13 | British Aircraft Corp Ltd | Spacecraft spin up and ejection apparatus |
US4554905A (en) * | 1984-04-05 | 1985-11-26 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Space probe/satellite ejection apparatus for spacecraft |
FR2705945B1 (en) * | 1993-06-04 | 1995-08-04 | Aerospatiale | Device for ejecting an object removably linked to a structure. |
FR2707750B1 (en) * | 1993-06-28 | 1995-09-22 | Aerospatiale | Device for ejecting, by pyrotechnic means, an object from a structure. |
JPH10147299A (en) * | 1996-11-20 | 1998-06-02 | Natl Space Dev Agency Japan<Nasda> | Hold releasing mechanism of rotary body structure |
-
2002
- 2002-02-14 GB GB0203513A patent/GB2385310A/en not_active Withdrawn
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109625339A (en) * | 2018-12-29 | 2019-04-16 | 西北工业大学 | A kind of micro-nano satellite separator of controllable rotating angular speed |
CN109625339B (en) * | 2018-12-29 | 2022-04-15 | 西北工业大学 | Micro-nano satellite separation device capable of controlling rotation angular velocity |
CN115057012A (en) * | 2022-08-03 | 2022-09-16 | 北京劢亚科技有限公司 | Multi-satellite chain type launching, locking, unlocking and ejecting mechanism |
CN115057012B (en) * | 2022-08-03 | 2022-10-25 | 北京劢亚科技有限公司 | Multi-satellite chain type launching, locking, unlocking and ejecting mechanism |
CN115009549A (en) * | 2022-08-09 | 2022-09-06 | 北京星河动力装备科技有限公司 | Locking and releasing mechanism, control method thereof and carrier rocket |
Also Published As
Publication number | Publication date |
---|---|
GB2385310A (en) | 2003-08-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |