Analysis of Efficiency of Systems for Control of the Thermal Regime of Spacecraft
- Авторлар: Delkov A.V.1, Kishkin A.A.1, Lavrov N.A.2, Tanasienko F.V.3
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Мекемелер:
- Siberian State Aerospace University
- Bauman Moscow State Technical University
- Reshetnev Information Satellite Systems
- Шығарылым: Том 51, № 9-10 (2016)
- Беттер: 714-719
- Бөлім: Article
- URL: https://journal-vniispk.ru/0009-2355/article/view/234229
- DOI: https://doi.org/10.1007/s10556-016-0110-z
- ID: 234229
Дәйексөз келтіру
Аннотация
Problems and the outlook for the development of effective systems of controlling the thermal regimes of spacecraft are considered. The process of creating and using the apparatus of mathematical modeling for the purpose of comparing the energy characteristics of different systems is described. The characteristics of forward and reverse working cycles of two-phase closed systems that control the thermal regimes are compared.
Авторлар туралы
A. Delkov
Siberian State Aerospace University
Хат алмасуға жауапты Автор.
Email: spsp99@mail.ru
Ресей, Krasnoyarsk
A. Kishkin
Siberian State Aerospace University
Email: lavrov@power.bmstu.ru
Ресей, Krasnoyarsk
N. Lavrov
Bauman Moscow State Technical University
Хат алмасуға жауапты Автор.
Email: lavrov@power.bmstu.ru
Ресей, Moscow
F. Tanasienko
Reshetnev Information Satellite Systems
Email: lavrov@power.bmstu.ru
Ресей, Zheznogorsk
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