Emerging Loop Heat Pipe Applications for Small-Sat, MARS Mission and ISS 2002-01-2464
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.
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. Download Citation
Author(s):
Frank Bodendieck, Reinhard Schlitt, Oliver Brand, Dirk Labuhn, Konstantin Goncharov, Vladimir Kalesnikovand Oleg Golovin
Affiliated:
OHB-System AG, TAIS
Pages: 11
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Control systems
Satellites
Spacecraft
Hardware
Tools and equipment
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