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Mathematical Model of Heat-Controlled Accumulator (HCA) for Microgravity Conditions

Journal Article
01-13-01-0001
ISSN: 1946-3855, e-ISSN: 1946-3901
DOI: https://doi.org/10.4271/01-13-01-0001
Published January 20, 2020 by SAE International in United States
Mathematical Model of Heat-Controlled Accumulator (HCA) for Microgravity Conditions
Sector:
Citation: Gorbenko, G., Koval, P., Yepifanov, K., Gakal, P. et al., "Mathematical Model of Heat-Controlled Accumulator (HCA) for Microgravity Conditions," SAE Int. J. Aerosp. 13(1):5-23, 2020, https://doi.org/10.4271/01-13-01-0001.
Language: English

References

  1. Nikonov , A.A. , Gorbenko , G.A. , and Blinkov , V.N. Heat-Exchange Loops with a Two-Phase Coolant for Spacecraft Thermal Control Systems Moscow TsNTI «Poisk» Publ. Ser. Raketnokosmicheskaya tekhnika, mashinostroenie 1991 302
  2. Basov , A.A. , Leksin , M.A. , Prokhorov , Yu.M. A Two-Phase Loop of Thermal Control System of Science-Power Module. Numerical Simulation of Hydraulic Characteristics Space Technique and Technology 2 17 80 89 2017
  3. Nigmatulin , R.I. Dynamics of Multiphase Media 1, 2 Hemisphere New York 1990 507 9780891163282
  4. Sementsov , A.N. 2003
  5. Yepifanov , K.S. and Semencov , A.N. 1999

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