FR2695907B1 - Vaisseau spatial avec panneaux thermiques et joints thermiques. - Google Patents
Vaisseau spatial avec panneaux thermiques et joints thermiques.Info
- Publication number
- FR2695907B1 FR2695907B1 FR9311165A FR9311165A FR2695907B1 FR 2695907 B1 FR2695907 B1 FR 2695907B1 FR 9311165 A FR9311165 A FR 9311165A FR 9311165 A FR9311165 A FR 9311165A FR 2695907 B1 FR2695907 B1 FR 2695907B1
- Authority
- FR
- France
- Prior art keywords
- thermal
- spaceship
- seals
- panels
- thermal panels
- 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.)
- Expired - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
- F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
- F28D15/0233—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes the conduits having a particular shape, e.g. non-circular cross-section, annular
-
- 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
- B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
- B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
- B64G1/503—Radiator panels
-
- 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
- B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
- B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
- B64G1/506—Heat pipes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
- F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
- F28D15/0266—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
- F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
- F28D15/0275—Arrangements for coupling heat-pipes together or with other structures, e.g. with base blocks; Heat pipe cores
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Sustainable Development (AREA)
- Biodiversity & Conservation Biology (AREA)
- Health & Medical Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- Environmental Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Details Of Aerials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/948,221 US5351746A (en) | 1992-09-21 | 1992-09-21 | Spacecraft thermal panels & make-break thermal joints |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2695907A1 FR2695907A1 (fr) | 1994-03-25 |
FR2695907B1 true FR2695907B1 (fr) | 1995-02-10 |
Family
ID=25487500
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9311165A Expired - Lifetime FR2695907B1 (fr) | 1992-09-21 | 1993-09-20 | Vaisseau spatial avec panneaux thermiques et joints thermiques. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5351746A (fr) |
JP (1) | JPH06191500A (fr) |
FR (1) | FR2695907B1 (fr) |
GB (1) | GB2270975B (fr) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3438087B2 (ja) * | 1995-02-16 | 2003-08-18 | アクトロニクス株式会社 | リボン状プレートヒートパイプ |
US5699982A (en) * | 1995-07-24 | 1997-12-23 | Martin Marietta Corporation | Spacecraft with heat dissipators mounted on thermally coupled shelves |
US5806803A (en) * | 1995-11-30 | 1998-09-15 | Hughes Electronics Corporation | Spacecraft radiator cooling system |
US5823477A (en) * | 1995-12-22 | 1998-10-20 | Hughes Electronics Corporation | Device and method for minimizing radiator area required for heat dissipation on a spacecraft |
US5806800A (en) * | 1995-12-22 | 1998-09-15 | Caplin; Glenn N. | Dual function deployable radiator cover |
DE19908683C2 (de) * | 1999-02-26 | 2001-03-01 | Dornier Gmbh | Radiatorstruktur eines Satelliten |
US6230790B1 (en) | 1999-05-10 | 2001-05-15 | Lockheed Martin Corporation | Thermal control system for spacecraft |
US6883588B1 (en) * | 2000-07-24 | 2005-04-26 | Space Systems/Loral, Inc. | Spacecraft radiator system using a heat pump |
JP2002046700A (ja) | 2000-07-24 | 2002-02-12 | Space Syst Loral Inc | 中温度作業流体を含む熱パイプを用いた宇宙船熱放散装置 |
US6854510B2 (en) * | 2001-04-24 | 2005-02-15 | Space Systems/Loral, Inc. | Spacecraft radiator system and method using cross-coupled deployable thermal radiators |
FR2840394B1 (fr) * | 2002-05-30 | 2004-08-27 | Cit Alcatel | Dispositif de transfert de chaleur pour satellite comprenant un evaporateur |
US20060076458A1 (en) * | 2004-02-19 | 2006-04-13 | Eads Astrium Ltd. | Payload module |
WO2010111364A1 (fr) * | 2009-03-24 | 2010-09-30 | Lockheed Martin Corporation | Système de dissipation de chaleur pour vaisseau spatial |
US9091489B2 (en) * | 2010-05-14 | 2015-07-28 | Paragon Space Development Corporation | Radiator systems |
US9238513B2 (en) | 2012-03-06 | 2016-01-19 | The Boeing Company | Spacecraft radiator panels |
US9403606B2 (en) * | 2012-03-06 | 2016-08-02 | The Boeing Company | Spacecraft radiator panels |
US9180984B2 (en) | 2012-05-11 | 2015-11-10 | The Boeing Company | Methods and apparatus for performing propulsion operations using electric propulsion systems |
US8915472B2 (en) * | 2012-05-11 | 2014-12-23 | The Boeing Company | Multiple space vehicle launch system |
CA2831309C (fr) * | 2012-12-04 | 2017-05-30 | The Boeing Company | Methodes et appareil d'execution des fonctions de propulsion a l'aide de dispositifs de propulsion electriques |
CN103274061B (zh) * | 2013-04-25 | 2016-08-10 | 上海卫星工程研究所 | 用于航天器的热管-流体回路耦合热辐射器 |
US9352856B1 (en) * | 2013-12-04 | 2016-05-31 | Space Systems/Loral, Llc | Axially grooved crossing heat pipes |
US10640237B2 (en) * | 2014-01-14 | 2020-05-05 | Made In Space, Inc. | Spacecraft having electronic components as structural members and related methods |
FR3031969B1 (fr) * | 2015-01-27 | 2017-01-27 | Airbus Defence & Space Sas | Satellite artificiel et procede de remplissage d'un reservoir de gaz propulsif dudit satellite artificiel |
EP3259189B1 (fr) * | 2015-06-02 | 2018-07-18 | Airbus Defence and Space SAS | Satellite artificiel |
WO2017169080A1 (fr) | 2016-03-31 | 2017-10-05 | 三菱電機株式会社 | Dispositif de dissipation thermique mettant en oeuvre un panneau à caloducs |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3749156A (en) * | 1972-04-17 | 1973-07-31 | E Powers | Thermal control system for a spacecraft modular housing |
US4162701A (en) * | 1977-11-21 | 1979-07-31 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal control canister |
DE2933088C2 (de) * | 1979-08-16 | 1982-07-01 | Dornier System Gmbh, 7990 Friedrichshafen | Temperaturstabilisierung für ein wärmeabgebendes Bauteil eines Satelliten |
JPS58219361A (ja) * | 1982-06-16 | 1983-12-20 | Hitachi Ltd | ヒ−トパイプ式太陽熱集熱器 |
JPS6383586A (ja) * | 1986-09-29 | 1988-04-14 | Nippon Telegr & Teleph Corp <Ntt> | ヒ−トパイプ埋め込みパネル |
US4880050A (en) * | 1988-06-20 | 1989-11-14 | The Boeing Company | Thermal management system |
US5372183A (en) * | 1991-08-22 | 1994-12-13 | Strickberger; Harold P. | Thermal control arrangements for a geosynchronous spacecraft |
-
1992
- 1992-09-21 US US07/948,221 patent/US5351746A/en not_active Expired - Lifetime
-
1993
- 1993-09-17 GB GB9319276A patent/GB2270975B/en not_active Expired - Fee Related
- 1993-09-20 FR FR9311165A patent/FR2695907B1/fr not_active Expired - Lifetime
- 1993-09-20 JP JP5232104A patent/JPH06191500A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
GB2270975A (en) | 1994-03-30 |
JPH06191500A (ja) | 1994-07-12 |
US5351746A (en) | 1994-10-04 |
GB9319276D0 (en) | 1993-11-03 |
GB2270975B (en) | 1996-04-03 |
FR2695907A1 (fr) | 1994-03-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property |