Demonstration of a two-stage Turbo-Brayton cryocooler for space applications.
Author(s) : ZAGAROLA M. V., BREEDLOVE J. J., KIRKCONNELL C. S., et al.
Summary
Turbo-Brayton cryocoolers have inherent technical advantages for many space applications because of their extremely low emitted vibration and simplicity of integration with payloads and spacecraft heat rejection systems.
Details
- Original title: Demonstration of a two-stage Turbo-Brayton cryocooler for space applications.
- Record ID : 2010-0694
- Languages: English
- Publication date: 2009
- Source: Source: Proc. 15th int. Cryocooler Conf., Boulder, CO/Cryocoolers 15
9 p.; fig.; photogr.; tabl.; 5 ref.
Links
Indexing
-
High rotational speed 2-5 K turbo-Brayton coole...
- Author(s) : DELCAYRE F., REALE S., MAROT G., et al.
- Date : 2002/07/22
- Languages : English
- Source: Proceedings of the nineteenth International Cryogenic Engineering Conference. ICEC 19.
View record
-
Development of advanced two-stage Stirling cryo...
- Author(s) : SATO Y., SUGITA H., KOMATSU K., et al.
- Date : 2009
- Languages : English
View record
-
Turbo-Brayton cryocoolers for space.
- Author(s) : ZAGAROLA M., McCORMICK J., SIXSMITH H., et al.
- Date : 2002/07/22
- Languages : English
- Source: Proceedings of the nineteenth International Cryogenic Engineering Conference. ICEC 19.
View record
-
Development of a two-stage high-temperature pul...
- Author(s) : CHARLES I., COYNEL A., DUVAL J. M., et al.
- Date : 2009
- Languages : English
View record
-
Cryogenic boil-off reduction system.
- Author(s) : PLACHTA D. W., GUZIK M. C.
- Date : 2014/03
- Languages : English
- Source: Cryogenics - vol. 60
View record