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Emerging Loop Heat Pipe Applications for Small-Sat, MARS Mission and ISS
ISSN: 0148-7191, e-ISSN: 2688-3627
Published July 15, 2002 by SAE International in United States
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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.
CitationBodendieck, 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.
- The Thermal Control Concept of the Mars Netlander Surface Module Serene F. Alet I. Schlitt R. Romberg O. Bodendieck F. Seiferlin K. Goncharov K. 31 th ICES paper 2001-01-2282 2001
- Thermal Performance Tests of Different Insulation Materials in a Simulated Mars Environment Schlitt R. Bodendieck F. Serene F. 4th Int. Symp. on Environemntal Testing for Space Programmes Liege, Belgium 12-14 June 2001