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9. Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (2); 49-52

Language: Russian

Annotation: The paper describes the experiments of cryogenic engine unit circulatory cooling system, considers the developed technique of circulation parameters evaluation and gives the comparison of calculated and experimental data on this system.

Key words:

Bibliography:
1. Evaluation of Parameters of Liquid Oxygen Circulation in Cryogenic LRPS Cooling System: Technical Note 22.8234.123 ST. Yuzhnoye SDO.
2. Kutepov A. M., Sterman L. S., Styushin N. G. Hydrodynamics and Heat Exchange at Vapor Formation. М., 1986.
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9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System
9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System
9.2.2017 Peculiarities of Development of Cryogenic Propulsion System Circulating Cooling System
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