DocumentCode :
1038838
Title :
Space environment testbed (SET): adaptable system for piggybacked satellite experiments
Author :
Fowler, Kim R. ; Frank, Laurence J. ; Williams, Robert L.
Author_Institution :
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
Volume :
53
Issue :
4
fYear :
2004
Firstpage :
1065
Lastpage :
1070
Abstract :
This paper introduces the concept of a flexible, adaptable subsystem for satellites that provides a platform for space-based experiments. The subsystem, called a carrier, comprises mechanical, electrical/electronic, thermal, data, and software components. We have performed a number of tradeoff studies and recommend a general type of architecture for the carrier that will satisfy many requirements and accommodate the constraints of space-based experimentation.
Keywords :
aerospace instrumentation; aerospace test facilities; space vehicles; adaptable subsystem; carrier; data components; electrical components; electronic components; mechanical components; piggybacked satellite experiments; software components; space environment testbed; space-based experiments; thermal components; Aircraft manufacture; Command and control systems; Computer architecture; Helium; Satellite ground stations; Space technology; Space vehicles; System testing; Telemetry; Temperature sensors; Satellites; adaptable subsystem; carrier; tradeoff studies;
fLanguage :
English
Journal_Title :
Instrumentation and Measurement, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9456
Type :
jour
DOI :
10.1109/TIM.2004.831497
Filename :
1315985
Link To Document :
بازگشت