The feasibility of cryogenic storage in space

International SAMPE Technical Conference

Volumn , Issue , 2004, Pages 613-624

  Wilson, Brian ^a   Mitchell, Ronald ^a   Arritt, Brandon ^b   Paul, Christopher ^b   Hender, Doug ^a  

^a Wilson Composite Technologies   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Aluminized Mylar; Foam Insulation; Linerless Composite Tanks; Long term Cryogenic Storage; MLI

Indexed keywords

ALUMINIZED MYLAR; FOAM INSULATION; LINERLESS COMPOSITE TANKS; LONG TERM CRYOGENIC STORAGE; MULTI LAYER INSULATION (MLI);

COMPOSITE MATERIALS; HEAT LOSSES; MICROCRACKING; PROBLEM SOLVING; STORAGE (MATERIALS); THERMAL INSULATION; THERMOANALYSIS;

CRYOGENICS;

EID: 4544320544     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. "Properties of Para-Hydrogen," Aerojet General Corporation Report 9050-6S, June 1963.
2. Gilmore, David G., Editor, "Satellite Thermal Control Handbook," The Aerospace Corporation Press, El Segundo, California, 1994.
3. Mohling, R. A., et al, "Multilayer Insulation Thick Blanket Performance Demonstration," AFAL TR-87-037 dated July 1987 from Ball Aerospace Systems Division in Boulder, CO.
4. Keller, C.W., Cunnington, G.R., and Glassford, A.P., "Thermal Performance of Multilayer Insulations, Final Report," prepared for NASA Lewis Research Center Contract NAS3-14377, Lockheed Missiles and Space Company, Sunnyvale, CA, 1971, NASA CR-134477.
5. Anderson, Dr. J., "Long Term Cryogenic Storage Demonstration," Phillips Laboratory Report PL-TR-93-3087 dated February 1994 from Martin Marietta Astronautics in Denver, CO.