DE69016770D1 - Abstrahlersystem für ein Raumfahrzeug. - Google Patents

Abstrahlersystem für ein Raumfahrzeug.

Info

Publication number
DE69016770D1
DE69016770D1 DE69016770T DE69016770T DE69016770D1 DE 69016770 D1 DE69016770 D1 DE 69016770D1 DE 69016770 T DE69016770 T DE 69016770T DE 69016770 T DE69016770 T DE 69016770T DE 69016770 D1 DE69016770 D1 DE 69016770D1
Authority
DE
Germany
Prior art keywords
spacecraft
radiator system
radiator
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 - Fee Related
Application number
DE69016770T
Other languages
English (en)
Other versions
DE69016770T2 (de
Inventor
Robert A Haslett
Robert L Kosson
Martin Solon
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.)
Grumman Corp
Original Assignee
Grumman Aerospace Corp
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 Grumman Aerospace Corp filed Critical Grumman Aerospace Corp
Application granted granted Critical
Publication of DE69016770D1 publication Critical patent/DE69016770D1/de
Publication of DE69016770T2 publication Critical patent/DE69016770T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00—Tubular elements; Assemblies of tubular elements
    • F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
    • F28F1/14—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending longitudinally
    • F28F1/22—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending longitudinally the means having portions engaging further tubular elements
    • 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
    • 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
    • B64G1/54—Protection against radiation
    • 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
    • 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
    • F28D15/04—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 tubes having a capillary structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/02—Constructions of heat-exchange apparatus characterised by the selection of particular materials of carbon, e.g. graphite
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2270/00—Thermal insulation; Thermal decoupling

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Health & Medical Sciences (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Toxicology (AREA)
  • Environmental Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • Biodiversity & Conservation Biology (AREA)
  • Sustainable Development (AREA)
  • Critical Care (AREA)
  • Emergency Medicine (AREA)
  • Geometry (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Thermal Insulation (AREA)
DE69016770T 1989-12-22 1990-12-18 Abstrahlersystem für ein Raumfahrzeug. Expired - Fee Related DE69016770T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/454,822 US5069274A (en) 1989-12-22 1989-12-22 Spacecraft radiator system

Publications (2)

Publication Number Publication Date
DE69016770D1 true DE69016770D1 (de) 1995-03-23
DE69016770T2 DE69016770T2 (de) 1995-09-14

Family

ID=23806257

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69016770T Expired - Fee Related DE69016770T2 (de) 1989-12-22 1990-12-18 Abstrahlersystem für ein Raumfahrzeug.

Country Status (4)

Country Link
US (1) US5069274A (de)
EP (1) EP0438938B1 (de)
JP (1) JP3048389B2 (de)
DE (1) DE69016770T2 (de)

Families Citing this family (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5372183A (en) * 1991-08-22 1994-12-13 Strickberger; Harold P. Thermal control arrangements for a geosynchronous spacecraft
DE4240082C1 (de) * 1992-11-28 1994-04-21 Erno Raumfahrttechnik Gmbh Wärmerohr
FR2735565B1 (fr) * 1995-06-13 1997-08-22 Aerospatiale Caloduc en materiau composite notamment pour panneau de satellite et son procede de fabrication
US7147045B2 (en) * 1998-06-08 2006-12-12 Thermotek, Inc. Toroidal low-profile extrusion cooling system and method thereof
US6935409B1 (en) 1998-06-08 2005-08-30 Thermotek, Inc. Cooling apparatus having low profile extrusion
US7305843B2 (en) 1999-06-08 2007-12-11 Thermotek, Inc. Heat pipe connection system and method
US6981322B2 (en) 1999-06-08 2006-01-03 Thermotek, Inc. Cooling apparatus having low profile extrusion and method of manufacture therefor
US6474074B2 (en) * 2000-11-30 2002-11-05 International Business Machines Corporation Apparatus for dense chip packaging using heat pipes and thermoelectric coolers
US6843308B1 (en) 2000-12-01 2005-01-18 Atmostat Etudes Et Recherches Heat exchanger device using a two-phase active fluid, and a method of manufacturing such a device
US6854510B2 (en) * 2001-04-24 2005-02-15 Space Systems/Loral, Inc. Spacecraft radiator system and method using cross-coupled deployable thermal radiators
US7198096B2 (en) * 2002-11-26 2007-04-03 Thermotek, Inc. Stacked low profile cooling system and method for making same
US9113577B2 (en) 2001-11-27 2015-08-18 Thermotek, Inc. Method and system for automotive battery cooling
US7857037B2 (en) 2001-11-27 2010-12-28 Thermotek, Inc. Geometrically reoriented low-profile phase plane heat pipes
FR2840394B1 (fr) * 2002-05-30 2004-08-27 Cit Alcatel Dispositif de transfert de chaleur pour satellite comprenant un evaporateur
DE10340092B4 (de) * 2003-08-30 2005-09-01 Ohb Orbitale Hochtechnologie Bremen--System Ag Sandwich Struktur mit kohlenfaserverstärkten Deckschichten und integrierten metallischen Kondensierrohren
US20050145371A1 (en) * 2003-12-31 2005-07-07 Eric Distefano Thermal solution for electronics cooling using a heat pipe in combination with active loop solution
US7983042B2 (en) * 2004-06-15 2011-07-19 Raytheon Company Thermal management system and method for thin membrane type antennas
US7143813B2 (en) * 2004-07-28 2006-12-05 The Boeing Company Foam bumper and radiator for a lightweight heat rejection system
US20060225870A1 (en) * 2005-04-12 2006-10-12 The Boeing Company Cooling apparatus, system, and associated method
DE102005039783B3 (de) * 2005-08-22 2007-03-22 Orbitale Hochtechnologie Bremen-System Ag Kohlenstofffaser-Sandwichstruktur mit integrierten metallischen Rohren
US20080115919A1 (en) * 2006-11-16 2008-05-22 Grant Allan Anderson Radiator Tube with Angled Flow Passage
FR2942774B1 (fr) * 2009-03-06 2011-05-06 Thales Sa Dispositif de controle thermique pour un engin spatial
US9109843B1 (en) * 2009-06-29 2015-08-18 Paragon Space Development Corporation Radiator systems
US8780559B2 (en) * 2011-12-29 2014-07-15 General Electric Company Heat exchange assembly for use with electrical devices and methods of assembling an electrical device
PL397894A1 (pl) 2012-01-25 2013-08-05 Krzysztof Bartoszewski Plat emisyjno-absorpcyjny, zwlaszcza plat grzewczo-chlodzacy
WO2013169774A2 (en) 2012-05-07 2013-11-14 Phononic Devices, Inc. Thermoelectric heat exchanger component including protective heat spreading lid and optimal thermal interface resistance
US20130291555A1 (en) 2012-05-07 2013-11-07 Phononic Devices, Inc. Thermoelectric refrigeration system control scheme for high efficiency performance
FR2997787B1 (fr) * 2012-11-07 2014-11-21 Technicatome Generateur nucleaire a radioisotope
US9315280B2 (en) * 2012-11-20 2016-04-19 Lockheed Martin Corporation Heat pipe with axial wick
US9426932B2 (en) * 2013-03-13 2016-08-23 Silicon Graphics International Corp. Server with heat pipe cooling
US9612920B2 (en) 2013-03-15 2017-04-04 Silicon Graphics International Corp. Hierarchical system manager rollback
DE102013107365C5 (de) * 2013-07-11 2021-03-25 Krauss-Maffei Wegmann Gmbh & Co. Kg Laserpanzerung
US9352856B1 (en) * 2013-12-04 2016-05-31 Space Systems/Loral, Llc Axially grooved crossing heat pipes
US9593871B2 (en) 2014-07-21 2017-03-14 Phononic Devices, Inc. Systems and methods for operating a thermoelectric module to increase efficiency
US10458683B2 (en) 2014-07-21 2019-10-29 Phononic, Inc. Systems and methods for mitigating heat rejection limitations of a thermoelectric module
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
US9868551B2 (en) * 2015-03-30 2018-01-16 Worldvu Satellites Limited Passive thermal system comprising combined heat pipe and phase change material and satellites incorporating same
US10118717B2 (en) * 2015-06-02 2018-11-06 Airbus Defence And Space Sas Artificial Satellite
CN109178348B (zh) * 2018-08-23 2020-10-20 北京航天长征飞行器研究所 一种与耐烧蚀材料耦合的脉动热管主动热防护结构
WO2020123523A1 (en) * 2018-12-10 2020-06-18 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Two-phase cooling in vascular composites using a pumped fluid loop
RU2716591C1 (ru) * 2019-04-11 2020-03-13 Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Радиатор-теплоаккумулятор пассивной системы терморегулирования космического объекта
US20220034607A1 (en) * 2020-07-28 2022-02-03 Kyle Borden Marquis Layered Radiator for Efficient Heat Rejection

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3211215A (en) * 1961-02-01 1965-10-12 Gen Motors Corp Heat exchangers suitable for space use
US4440215A (en) * 1971-02-08 1984-04-03 Q-Dot Corporation Heat pipe
GB1455002A (en) * 1973-01-08 1976-11-10 Redpoint Ltd Heat sink assembly
SU518614A1 (ru) * 1975-01-13 1976-06-25 Московская кондитерская фабрика "Большевик" Тепловой диод
US4351388A (en) * 1980-06-13 1982-09-28 Mcdonnell Douglas Corporation Inverted meniscus heat pipe
US4470451A (en) * 1981-03-16 1984-09-11 Grumman Aerospace Corporation Dual axial channel heat pipe
JPS62242794A (ja) * 1986-04-15 1987-10-23 Komatsu Ltd 熱交換器

Also Published As

Publication number Publication date
JPH04208393A (ja) 1992-07-30
EP0438938A3 (en) 1991-10-09
DE69016770T2 (de) 1995-09-14
EP0438938A2 (de) 1991-07-31
US5069274A (en) 1991-12-03
JP3048389B2 (ja) 2000-06-05
EP0438938B1 (de) 1995-02-08

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee