JPH0318000U - - Google Patents
Info
- Publication number
- JPH0318000U JPH0318000U JP7893489U JP7893489U JPH0318000U JP H0318000 U JPH0318000 U JP H0318000U JP 7893489 U JP7893489 U JP 7893489U JP 7893489 U JP7893489 U JP 7893489U JP H0318000 U JPH0318000 U JP H0318000U
- Authority
- JP
- Japan
- Prior art keywords
- satellite
- motor
- apogee
- apogee motor
- central cylinder
- 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
- 238000000926 separation method Methods 0.000 claims description 2
- 238000002485 combustion reaction Methods 0.000 claims 1
- 239000003721 gunpowder Substances 0.000 claims 1
- 239000003380 propellant Substances 0.000 claims 1
- 230000008646 thermal stress Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
- 239000002360 explosive Substances 0.000 description 1
Landscapes
- Braking Arrangements (AREA)
Description
第１図は本考案の一実施例を示す構成図、第２
図は従来の人工衛星の衛星構体とアポジキツクモ
ータの取付け部を示す構成図である。図に於いて
、１……アポジキツクモータ、２……セントラル
シリンダ、３……取付けフランジ、４……分離ボ
ルト部、５……火薬ラインを示している。なお、
図中同一符号は、同一または相当部分を示す。
Fig. 1 is a configuration diagram showing one embodiment of the present invention;
The figure is a configuration diagram showing the satellite structure of a conventional artificial satellite and the attachment part of the apogeometric motor. In the figure, 1...Apostatic motor, 2...Central cylinder, 3...Mounting flange, 4...Separation bolt section, 5...Explosive line. In addition,
The same reference numerals in the figures indicate the same or corresponding parts.
Claims (1)
ントラルシリンダにアポジキツクモータを固定し
ている爆管応用分離ボルトと、この分離ボルトの
爆管に、アポジキツクモータが完全に燃焼した段
階で点火する火薬ラインを備え、アポジキツクモ
ータを、完全に燃焼した段階ですみやかに衛星本
体より分離することにより、燃焼後のアポジキツ
クモータが衛星本体へ与える熱的ストレスを無く
し、かつ静止軌道上に於ける衛星質量軽減による
二次推進系推薬の節約を計ることを特徴とした人
工衛星。 A central cylinder that is the satellite structure, a detonator separation bolt that fixes the apogee motor to the central cylinder, and a gunpowder line that ignites the apogee motor when the apogee motor is completely combusted. By quickly separating the apogeometric motor from the satellite body after it has completely burned out, we can eliminate the thermal stress that the apogee motor exerts on the satellite body after combustion, and reduce the mass of the satellite in geostationary orbit. An artificial satellite characterized by saving propellant in the secondary propulsion system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7893489U JPH0318000U (en) | 1989-07-04 | 1989-07-04 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7893489U JPH0318000U (en) | 1989-07-04 | 1989-07-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0318000U true JPH0318000U (en) | 1991-02-21 |
Family
ID=31622647
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7893489U Pending JPH0318000U (en) | 1989-07-04 | 1989-07-04 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0318000U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05146781A (en) * | 1991-11-27 | 1993-06-15 | Sharp Corp | Electrolytic water generator |
| JP2002539876A (en) * | 1999-03-26 | 2002-11-26 | シェフン コーポレイション | Method of making improved grater and grater |
-
1989
- 1989-07-04 JP JP7893489U patent/JPH0318000U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05146781A (en) * | 1991-11-27 | 1993-06-15 | Sharp Corp | Electrolytic water generator |
| JP2002539876A (en) * | 1999-03-26 | 2002-11-26 | シェフン コーポレイション | Method of making improved grater and grater |
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