JPS58194700A - 宇宙飛行体の温度制御装置 - Google Patents
宇宙飛行体の温度制御装置Info
- Publication number
- JPS58194700A JPS58194700A JP57079029A JP7902982A JPS58194700A JP S58194700 A JPS58194700 A JP S58194700A JP 57079029 A JP57079029 A JP 57079029A JP 7902982 A JP7902982 A JP 7902982A JP S58194700 A JPS58194700 A JP S58194700A
- Authority
- JP
- Japan
- Prior art keywords
- temperature
- spacecraft
- fluid
- spin
- pipe
- 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
- 239000012530 fluid Substances 0.000 claims description 14
- 230000001133 acceleration Effects 0.000 claims description 6
- 230000008878 coupling Effects 0.000 claims description 2
- 238000010168 coupling process Methods 0.000 claims description 2
- 238000005859 coupling reaction Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 238000012935 Averaging Methods 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
Landscapes
- Physical Or Chemical Processes And Apparatus (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57079029A JPS58194700A (ja) | 1982-05-11 | 1982-05-11 | 宇宙飛行体の温度制御装置 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57079029A JPS58194700A (ja) | 1982-05-11 | 1982-05-11 | 宇宙飛行体の温度制御装置 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS58194700A true JPS58194700A (ja) | 1983-11-12 |
JPS6241920B2 JPS6241920B2 (enrdf_load_stackoverflow) | 1987-09-04 |
Family
ID=13678499
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57079029A Granted JPS58194700A (ja) | 1982-05-11 | 1982-05-11 | 宇宙飛行体の温度制御装置 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58194700A (enrdf_load_stackoverflow) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62264511A (ja) * | 1986-05-12 | 1987-11-17 | 株式会社 潤工社 | 宇宙空間におけるケ−ブルの保護方法 |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62163617U (enrdf_load_stackoverflow) * | 1986-04-07 | 1987-10-17 |
-
1982
- 1982-05-11 JP JP57079029A patent/JPS58194700A/ja active Granted
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62264511A (ja) * | 1986-05-12 | 1987-11-17 | 株式会社 潤工社 | 宇宙空間におけるケ−ブルの保護方法 |
Also Published As
Publication number | Publication date |
---|---|
JPS6241920B2 (enrdf_load_stackoverflow) | 1987-09-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Steinfeld et al. | Optimum aperture size and operating temperature of a solar cavity-receiver | |
US8967547B2 (en) | Spacecraft east-west radiator assembly | |
US3152774A (en) | Satellite temperature stabilization system | |
JP6302603B2 (ja) | 宇宙船 | |
US6073887A (en) | High power spacecraft with full utilization of all spacecraft surfaces | |
CN105346737A (zh) | 一种geo轨道卫星激光装置热控制方法 | |
Novak et al. | Development of a thermal control architecture for the Mars Exploration Rovers | |
US3451641A (en) | Thermoelectric conversion system | |
JPS58194700A (ja) | 宇宙飛行体の温度制御装置 | |
Hawarden et al. | Optimised radiative cooling of infrared space telescopes and applications to possible missions | |
Kerslake et al. | Two-dimensional model of a space station freedom thermal energy storage canister | |
Bulut et al. | Optimized analytical solution of platform panel radiative area dimensioning of geostationary communications satellites: a practical approach | |
US3606207A (en) | Reentry vehicle for thermoelectric generator | |
De | Disequilibrium condensation environments in space: A frontier in thermodynamics | |
Mishra | Thermal Control Subsystem for CubeSat in Low Earth Orbit | |
Neuberger et al. | Advanced geosynchronous studies imager thermal design | |
RU2034756C1 (ru) | Система термостатирования оборудования негерметичного теплоизолированного контейнера космического аппарата | |
Glassman et al. | Thermodynamic characteristics of brayton cycles for space power | |
Carfi et al. | A comparative thermal study of a GEO satellite for geostationary transfer orbit and mission orbit | |
Jenness | Radiative cooling of satellite-borne electronic components | |
Rossi | A study of advanced thermal protection systems | |
Walker et al. | The impact of the lunar thermal environment on the design of telescopes for lunar surface operation | |
Katzoff | of a Large Orbiting Telescope | |
WISE et al. | Thermal design verification of a high-power direct broadcast satellite | |
TIWARI et al. | Influence of nonequilibrium radiation and shape change on aerothermal environment of Jovian entry body[Final Report, 1 Aug. 1979- 29 Feb. 1980] |