Emerging Loop Heat Pipe Applications for Small-Sat, MARS Mission and ISS

2002-01-2464

07/15/2002

Event
International Conference On Environmental Systems
Authors Abstract
Content
Loop Heat Pipes (LHP) emerge as standard equipment for spacecraft thermal control. Based on a co-operation agreement between TAIS, Moscow and OHB-System AG, Bremen several thermal control projects for Mars mission, ISS and small satellites have been initiated, which are all based on loop heat pipes. The thermal control systems, described in this paper, are currently under development or hardware manufacturing. The paper will detail the application scenario, development steps and first test results.
Meta TagsDetails
DOI
https://doi.org/10.4271/2002-01-2464
Pages
11
Citation
Bodendieck, F., Schlitt, R., Brand, O., Labuhn, D. et al., "Emerging Loop Heat Pipe Applications for Small-Sat, MARS Mission and ISS," SAE Technical Paper 2002-01-2464, 2002, https://doi.org/10.4271/2002-01-2464.
Additional Details
Publisher
Published
Jul 15, 2002
Product Code
2002-01-2464
Content Type
Technical Paper
Language
English