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Determination of the Heat-Controlled Accumulator Volume for the Two-Phase Thermal Control Systems of Spacecraft

Journal Article
01-17-01-0008
ISSN: 1946-3855, e-ISSN: 1946-3901
Published September 29, 2023 by SAE International in United States
Determination of the Heat-Controlled Accumulator Volume for the
                    Two-Phase Thermal Control Systems of Spacecraft
Sector:
Citation: Hodunov, A., Gorbenko, G., Turna, R., and Koval, P., "Determination of the Heat-Controlled Accumulator Volume for the Two-Phase Thermal Control Systems of Spacecraft," SAE Int. J. Aerosp. 17(1):123-130, 2024, https://doi.org/10.4271/01-17-01-0008.
Language: English

References

  1. NASA 2015
  2. Nikonov , A.A. , Gorbenko , G.A. , and Blinkov , V.N. Teploobmennye kontury s dvukhfaznym teplonositelem dlya sistem termoregulirovaniya kosmicheskikh apparatov [Heat Exchanging Loops with a Two-Phase Coolant for Spacecraft Thermal Control Systems] Moscow “Rocket and Space Technology, Machine Building” Publ. 1991
  3. Edelstein , F. , Liandris , M. , and Rankin , J. Thermal Test Results of the Two-Phase Thermal Bus Technology Demonstration Loop 22nd Thermophysics Conference Reston, VA American Institute of Aeronautics and Astronautics 1987 10.2514/6.1987-1627
  4. Gorbenko , G. , Gakal , P. , Turna , R. , and Hodunov , A. Retrospective Review of a Two-Phase Mechanically Pumped Loop for Spacecraft Thermal Control Systems Journal of Mechanical Engineering 24 4 2021 27 37 10.15407/pmach2021.04.027
  5. Epifanov , K.S. and Semencov , A.N. Identifikatsiyamodeli teplovogo gidroakkumulyatora kontura teploperenosa Rossiyskogo segmenta Mezhdunarodnoykosmicheskoy stantsii ‘Alfa’ [Identification of the Model of Heat Controlled Accumulator of the Heat Transfer Loop of the Russian Segment of the InternationalSpace Station ‘Alpha’] Aviacijno-kosmicna tehnika itehnologia – Aerospace Technic and Technology 9 1999 527 533
  6. Meng , Q. et al. Experimental Study on the Transient Behaviors of Mechanically Pumped Two-Phase Loop-with a Novel Accumulator for Thermal Control of Spacecamera Payload Applied Thermal Engineering 179 2020 115714 10.1016/j.applthermaleng.2020.115714
  7. 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 2020 5 23 https://doi.org/10.4271/01-13-01-0001
  8. Hodunov , A. , Gorbenko , G. , and Gakal , P. The Calculation of the Heat Control Accumulator Volume of Two-Phase Heat Transfer Loop of a Spacecraft Thermal Control System Aerospace Technic and Technology 5 2021 15 23 10.32620/aktt.2021.5.0
  9. SIEMENS 2020
  10. Chisholm , D. Two-Phase Flow in Pipelines and Heat Exchangers London G. Godwin in Association with Institution of Chemical Engineers 1983

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