Passive ZBO storage of liquid hydrogen and liquid oxygen applied to space science mission concepts

Cryogenics

Volumn 46, Issue 2-3, 2006, Pages 89-97

  Plachta, D W ^a   Christie, R J ^b   Jurns, J M ^c   Kittel, P ^d  

^a NASA GLENN RESEARCH CENTER   (United States)

^b ZIN Technologies Inc   (United States)

^c QSS GROUP INC   (United States)

^d NONE

Author keywords

Heat transfer; Hydrogen; Oxygen; Space cryogenics

Indexed keywords

CRYOGENICS; HEAT TRANSFER; OXYGEN; PROPELLANTS; PROPULSION; SPACE RESEARCH;

CRYOCOOLERS; SPACE CRYOGENICS; SURFACE TEMPERATURES;

HYDROGEN;

EID: 33244476098     PISSN: 00112275     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.cryogenics.2005.11.012     Document Type: Conference Paper

References (11)

1. Guernsey C, Baker R, Plachta D, Kittel P, Christie R, Jurns J. Cryogenic propulsion with zero-boil-off storage applied to outer planetary exploration. JPL D-31783, April, 2005.
2. Plachta D, Christie R, Jurns J, Kittel P. ZBO cryogenic propellant storage applied to a Mars sample return mission concept. Presented at the Cryogenic Engineering Conference, Keystone, Colorado, August 31, 2005.
3. Plachta D, Kittel P. An updated zero boil-off cryogenic propellant storage analysis applied to upper stages or depots in an LEO environment. NASA TM-2003-211691. Presented at the 2002 AIAA Joint Propulsion Conference, Indianapolis, Indiana, July 8, 2002.
4. P. Kittel, and D.W. Plachta Propellant preservation for Mars missions Adv cryo engin vol. 45 2000 Kluwer New York 443
5. C. Lin, N. Van Dresar, and M. Hasan Pressure control analysis of cryogenic storage systems J Propul Power 20 3 2004
6. Thermal performance of multilayer insulations. NASA CR-134477, April 1974.
7. Martin J, Hastings L. Large-scale liquid hydrogen testing of a variable density multilayer insulation with a foam substrate. NASA TM-2001-211089.
8. I.E. Spradley, and R.T. Parmley Design and test of a modified passive orbital disconnect strut Adv cryo engin vol. 33 1988 Plenum New York 935
9. R.G. Ross Estimation of thermal conduction loads for structural supports of cryogenic spacecraft assemblies Cryogenics 44 2004 421
10. DeWitt R. Boyle R. Thermal performance of an integrated thermal protection system for long-term storage of cryogenic propellants in space. NASA TN D-8320, NASA LeRC, May 1977.
11. Plachta D. Results of an advanced development zero boil-off cryogenic propellant storage test. NASA TM-2004-213390.