Evaluation of supercritical cryogen storage and transfer systems forfuture NASA missions

Journal of Propulsion and Power

Volumn 8, Issue 2, 1992, Pages 332-338

  Arif, Hugh ^a   Aydelott, John C ^a   Chato, David J ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CRYOGENICS;

FLUID STORAGE SYSTEMS; SUPERCRITICAL FLUID STORAGE; SUPERCRITICALITY;

PROPELLANTS;

EID: 0026839877     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.23482     Document Type: Article

References (6)

1. Allgeier, R. K., Jr., Davis, M. L., Rodgers, T. G., and Rysavy, G. “The Development of Cryogenic Storage Systems for Space Flight,’ NASA SP-247, 1970.
2. Orbital Transfer Vehicle, Concept Definition, and Systems Analysis Study, Executive Summary,” D180-29108-11-1, NAS8-36107, Boeing Aerospace Co., Seattle, WA, March 1988.
3. McCarty, R. D., and Weber, L. A., “Thermophysical Properties of Parahydrogen from the Freezing Liquid Line to 5000R for Pressure to 10,000 Psia,” NBS-TN-617, National Bureau of Standards, NASA CR-12770, April 1972.
4. Roger, H. M., and Weber, L. A., “ASRDI Oxygen Technology Survey, Vol. I; Thermophysical Properties,” NASA SP-3071, 1972.
5. Timoshenko, S., Theory of Plates and Shells, 2nd ed., McGraw- Hill, New York, 1959, Chap. 15, p. 481.
6. Morris, E. E., “Commercial Filament Wound Pressure Vessels for Military and Aerospace Applications,” Society of Automotive Engineers, Paper 811093, Oct. 1981.