Share Email Print
cover

Proceedings Paper

University Nanosat System thermal design, analysis, and testing
Author(s): Charlotte Gerhart
Format Member Price Non-Member Price
PDF $14.40 $18.00

Paper Abstract

Thermal design for space systems is an iterative process that balances the temperature requirements for all mission phases with the available resources. Secondary payloads often have to be designed for a wide range of conditions available on various launch platforms, without the benefit of additional resources such as power or thermal shielding. This paper will discuss the thermal design, analysis, and thermal vacuum testing of a small satellite payload that was initially intended for launch from the US Space Shuttle and eventually launched on the EELV Heavy demonstration in December 2004.

Paper Details

Date Published: 31 May 2006
PDF: 11 pages
Proc. SPIE 6221, Modeling, Simulation, and Verification of Space-based Systems III, 62210A (31 May 2006); doi: 10.1117/12.667770
Show Author Affiliations
Charlotte Gerhart, Air Force Research Lab. (United States)


Published in SPIE Proceedings Vol. 6221:
Modeling, Simulation, and Verification of Space-based Systems III
Pejmun Motaghedi, Editor(s)

© SPIE. Terms of Use
Back to Top