Mathematical model and experimental results for cryogenic densification and sub-cooling using a submerged cooling source-Reference-Cited by-同舟云学术

Mathematical model and experimental results for cryogenic densification and sub-cooling using a submerged cooling source

Published:2012-04 Issue:4-6 Volume:52 Page:262-267
ISSN:0011-2275
Container-title:Cryogenics
language:en
Short-container-title:Cryogenics

Author:

Partridge J.K.,Tuttle J.W.,Notardonato W.U.,Johnson W.L.

Publisher

Elsevier BV

Subject

General Physics and Astronomy,General Materials Science

Reference9 articles.

1. Fazah MM. STS propellant densification feasibility study data book: NASA technical memorandum 108467. Marshall Space Flight Center, AL: NASA; 1994.

2. Greene William D, Vaughn David A. Simulation and testing of in-tank propellant densification for launch vehicles. AIAA; 1998. p. 3688.

3. Haberbusch MS et al. Modeling the RL10 with densified liquid hydrogen and oxygen propellants. AIAA; 2002. p. 3597.

4. Lak T, Lozano M, Tomsik T. Advancement in cryogenic propulsion system performance through propellant densification. AIAA; 1996. p. 3123.

5. Lak TI, Lozano ME, Neary DA. Propellant densification without use of rotating machinery. AIAA; 2002. p. 3599–608.

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