Analysis of Efficiency of Systems for Control of the Thermal Regime of Spacecraft
- Авторы: Delkov A.V.1, Kishkin A.A.1, Lavrov N.A.2, Tanasienko F.V.3
-
Учреждения:
- Siberian State Aerospace University
- Bauman Moscow State Technical University
- Reshetnev Information Satellite Systems
- Выпуск: Том 51, № 9-10 (2016)
- Страницы: 714-719
- Раздел: Article
- URL: https://journal-vniispk.ru/0009-2355/article/view/234229
- DOI: https://doi.org/10.1007/s10556-016-0110-z
- ID: 234229
Цитировать
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.
Об авторах
A. Delkov
Siberian State Aerospace University
Автор, ответственный за переписку.
Email: spsp99@mail.ru
Россия, Krasnoyarsk
A. Kishkin
Siberian State Aerospace University
Email: lavrov@power.bmstu.ru
Россия, Krasnoyarsk
N. Lavrov
Bauman Moscow State Technical University
Автор, ответственный за переписку.
Email: lavrov@power.bmstu.ru
Россия, Moscow
F. Tanasienko
Reshetnev Information Satellite Systems
Email: lavrov@power.bmstu.ru
Россия, Zheznogorsk
Дополнительные файлы
