JPS5992100U - Spacecraft separation mechanism - Google Patents
Spacecraft separation mechanismInfo
- Publication number
- JPS5992100U JPS5992100U JP18894282U JP18894282U JPS5992100U JP S5992100 U JPS5992100 U JP S5992100U JP 18894282 U JP18894282 U JP 18894282U JP 18894282 U JP18894282 U JP 18894282U JP S5992100 U JPS5992100 U JP S5992100U
- Authority
- JP
- Japan
- Prior art keywords
- spacecraft
- main body
- separation mechanism
- protrusion
- lever
- 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.)
- Granted
Links
Landscapes
- Manipulator (AREA)
- Casings For Electric Apparatus (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第1図は本考案の実施例の部分破砕正面図、第2図は第
1図の一部分を拡大した側面図である。
図において1・・・宇宙飛行体、2・・・親機、3・・
・保持枠、4.7・・・L字形テコ、5,8・・・勃興
、6゜9.21・・・バネ、10・・・ピン、11・・
・保持具、12.13・・・モータ、14.15・・・
紐、16゜17・・・回転の向きを示す矢印、18.
19. 20・・・保持点である。FIG. 1 is a partially exploded front view of an embodiment of the present invention, and FIG. 2 is an enlarged side view of a portion of FIG. In the diagram, 1... spacecraft, 2... main aircraft, 3...
・Holding frame, 4.7...L-shaped lever, 5,8...Erection, 6°9.21...Spring, 10...Pin, 11...
・Holder, 12.13...Motor, 14.15...
String, 16°17...Arrow indicating direction of rotation, 18.
19. 20... is a holding point.
Claims (1)
一端の突起部を支える支持部材と、一端が前記宇宙飛行
体の他端の突起部を支持でき前記本体に設けられた支点
に支えられたてこ状部材と、このてこ状部材の他端を引
張って移動させることにより前記他端の突起部の前記本
体べの支持を解放する解放手段と、この解放手段を駆動
する電動モータと、この電動モータに回転指令を与える
指令手段と、前記宇宙飛行体の両突起部間の一部を押圧
するように前記本体に設けられたばね状部材とを含む宇
宙飛行体の分離機構。a support member provided on a main body holding a spacecraft and supporting a protrusion at one end of the spacecraft; and a support member having one end capable of supporting a protrusion at the other end of the spacecraft and supported by a fulcrum provided on the main body. A lever-like member, a release means for releasing the support of the main body portion of the protrusion at the other end by pulling and moving the other end of the lever-like member, an electric motor for driving the release means; A separation mechanism for a spacecraft, including a command means for giving a rotation command to an electric motor, and a spring-like member provided on the main body so as to press a part between both protrusions of the spacecraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18894282U JPS5992100U (en) | 1982-12-14 | 1982-12-14 | Spacecraft separation mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18894282U JPS5992100U (en) | 1982-12-14 | 1982-12-14 | Spacecraft separation mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5992100U true JPS5992100U (en) | 1984-06-22 |
| JPS637600Y2 JPS637600Y2 (en) | 1988-03-04 |
Family
ID=30407484
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP18894282U Granted JPS5992100U (en) | 1982-12-14 | 1982-12-14 | Spacecraft separation mechanism |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5992100U (en) |
-
1982
- 1982-12-14 JP JP18894282U patent/JPS5992100U/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS637600Y2 (en) | 1988-03-04 |
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