Two-phase flow characteristics of liquid oxygen flow in low pressure liquid rocket engine

Author:

Cho Namkyung,Kim Seunghan,Kim Youngmog,Jeong Sangkwon,Jung Jeheon

Publisher

Elsevier BV

Subject

General Physics and Astronomy,General Materials Science

Reference9 articles.

1. Woodward RD. Injector Research for Shuttle OMS Upgrade Using LOX/Ethanol Propellants. In: 34th AIAA/ASME/SAE/SEE Joint Propulsion Conference & Exhibition, Cleveland, OH, July 13–15, 1998. p. 1–8

2. Application of combustion stabilization devices to liquid rocket engine;Sohn;J. Korean Soc. Aeronaut. Space Sci.,2003

3. Modeling of cryogenic transfer line cool down;Hasan;Adv. Cryogenic Eng.,2000

4. Cryogenic heat transfer;Clark;Adv. Heat Transfer,1965

5. Cryogenic systems;Barron,1985

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