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On-Orbit Thermal Performance of the TES Instrument-Three Years in Space

Journal Article
2008-01-2118
ISSN: 1946-3855, e-ISSN: 1946-3901
Published June 29, 2008 by SAE International in United States
On-Orbit Thermal Performance of the TES Instrument-Three Years in Space
Sector:
Citation: Rodriguez, J., Na-Nakornpanom, A., Rivera, J., Mireles, V. et al., "On-Orbit Thermal Performance of the TES Instrument-Three Years in Space," SAE Int. J. Aerosp. 1(1):364-375, 2009, https://doi.org/10.4271/2008-01-2118.
Language: English

References

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  4. Formation Flying: The Afternoon A-Train Satellite Constellation. NASA Fact Sheet FS-2003-1-053-GSFC 2003
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  10. Ross R.G. Jr. “Cryocooler Load Increase due to External Contamination of Low-e Cryogenic Surfaces,” Cryocoolers 12, Plenum Publishing Corp. NY 2002 727 736
  11. Rodriguez J.I. Na-Nakornpanom A. Rivera J.G. Mireles V. Tseng H “On-Orbit Performance of the TES Loop Heat Pipe Heat Rejection System,” SAE Paper No. 2008-01-2000 July 2008

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