FR2463058B1 - INSTALLATION PROVIDING WITHOUT ADJUSTMENT THE EXHAUST OF THE HEAT AND THE STABILIZATION OF THE TEMPERATURE - Google Patents

INSTALLATION PROVIDING WITHOUT ADJUSTMENT THE EXHAUST OF THE HEAT AND THE STABILIZATION OF THE TEMPERATURE

Info

Publication number
FR2463058B1
FR2463058B1 FR8015032A FR8015032A FR2463058B1 FR 2463058 B1 FR2463058 B1 FR 2463058B1 FR 8015032 A FR8015032 A FR 8015032A FR 8015032 A FR8015032 A FR 8015032A FR 2463058 B1 FR2463058 B1 FR 2463058B1
Authority
FR
France
Prior art keywords
stabilization
exhaust
adjustment
heat
temperature
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
Application number
FR8015032A
Other languages
French (fr)
Other versions
FR2463058A1 (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dornier System GmbH
Original Assignee
Dornier System GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Dornier System GmbH filed Critical Dornier System GmbH
Publication of FR2463058A1 publication Critical patent/FR2463058A1/en
Application granted granted Critical
Publication of FR2463058B1 publication Critical patent/FR2463058B1/en
Expired legal-status Critical Current

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
    • B64G1/46—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
    • 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
    • B64G1/52—Protection, safety or emergency devices; Survival aids
    • B64G1/58—Thermal protection, e.g. heat shields
    • 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
FR8015032A 1979-08-16 1980-07-02 INSTALLATION PROVIDING WITHOUT ADJUSTMENT THE EXHAUST OF THE HEAT AND THE STABILIZATION OF THE TEMPERATURE Expired FR2463058B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19792933088 DE2933088C2 (en) 1979-08-16 1979-08-16 Temperature stabilization for a heat-emitting component of a satellite

Publications (2)

Publication Number Publication Date
FR2463058A1 FR2463058A1 (en) 1981-02-20
FR2463058B1 true FR2463058B1 (en) 1985-06-21

Family

ID=6078533

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8015032A Expired FR2463058B1 (en) 1979-08-16 1980-07-02 INSTALLATION PROVIDING WITHOUT ADJUSTMENT THE EXHAUST OF THE HEAT AND THE STABILIZATION OF THE TEMPERATURE

Country Status (2)

Country Link
DE (1) DE2933088C2 (en)
FR (1) FR2463058B1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4933951A (en) * 1988-08-10 1990-06-12 Ltv Aerospace And Defense Company Minimum thermal environment sensor
US5305973A (en) * 1989-12-07 1994-04-26 Rockwell International Corporation Temperature normalized structure
US5372183A (en) * 1991-08-22 1994-12-13 Strickberger; Harold P. Thermal control arrangements for a geosynchronous spacecraft
US5332030A (en) * 1992-06-25 1994-07-26 Space Systems/Loral, Inc. Multi-directional cooler
US5310141A (en) * 1992-09-21 1994-05-10 General Electric Co. Battery thermal control arrangement
US5351746A (en) * 1992-09-21 1994-10-04 General Electric Co. Spacecraft thermal panels & make-break thermal joints
JPH0853100A (en) * 1994-08-10 1996-02-27 Mitsubishi Electric Corp Honeycomb sandwhich panel with heat pipe embedded in it
US5806803A (en) * 1995-11-30 1998-09-15 Hughes Electronics Corporation Spacecraft radiator cooling system
US5823476A (en) * 1995-12-22 1998-10-20 Hughes Electronics Corporation Device and method for equalizing heat dissipation between multiple radiators on a spacecraft
FR2759345B1 (en) 1997-02-10 1999-04-16 Aerospatiale STABILIZED GEOSTATIONARY SATELLITE THREE AXES WITH IMPROVED THERMAL CONTROL
US6073887A (en) * 1997-07-16 2000-06-13 Space Systems/Loral, Inc. High power spacecraft with full utilization of all spacecraft surfaces
US6938679B1 (en) * 1998-09-15 2005-09-06 The Boeing Company Heat transport apparatus
US9376222B2 (en) * 2014-11-11 2016-06-28 NovaWurks, Inc. Method of cooling satlet electronics
US10696429B2 (en) 2017-02-03 2020-06-30 The Boeing Company Dual condenser loop heat pipe for satellites with sun-normal radiators

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3152774A (en) * 1963-06-11 1964-10-13 Wyatt Theodore Satellite temperature stabilization system
US3749156A (en) * 1972-04-17 1973-07-31 E Powers Thermal control system for a spacecraft modular housing
LU72212A1 (en) * 1975-04-04 1977-02-02

Also Published As

Publication number Publication date
DE2933088C2 (en) 1982-07-01
DE2933088A1 (en) 1981-02-26
FR2463058A1 (en) 1981-02-20

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Legal Events

Date Code Title Description
ST Notification of lapse