High-pressure cryogenic hydrogen storage system for a Mars sample return mission.
Author(s) : MÜLLER P. J., BATTY J. C., ZUBRIN R. M.
Summary
One method to reduce the cost of space missions is to use indigenous Martian carbon dioxide, combined with hydrogen brought from Earth, to generate oxygen and methane propellant for the return trip to Earth. The paper uses the results from a computer simulation program to examine the feasibility of allowing the pressure in the tanks to reach maximum pressures from 3.4 to 13.8 megapascals.
Details
- Original title: High-pressure cryogenic hydrogen storage system for a Mars sample return mission.
- Record ID : 1997-2679
- Languages: English
- Source: 1995 Space Cryogenics Workshop.
- Publication date: 1996/10
Links
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Indexing
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Space-based liquid hydrogen propellant storage ...
- Author(s) : LIGGETT M. W.
- Date : 1993/04
- Languages : English
- Source: Cryogenics - vol. 33 - n. 4
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The development of methods and means of evacuat...
- Author(s) : CHEREMNYKH O. Y.
- Date : 2012/09/11
- Languages : English
- Source: Cryogenics 2012. Proceedings of the 12th IIR International Conference: Dresden, Germany, September 11-14, 2012.
- Formats : PDF
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THE STATUS OF HANDLING AND STORAGE TECHNIQUES F...
- Author(s) : PESCHKA W.
- Date : 1987
- Languages : English
- Source: Int. J. Hydrog. Energy - vol. 12 - n. 11
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BEARINGS FOR CRYOGENIC TURBOPUMPS.
- Author(s) : KRISHNA-REDDY M., KANAKA-RAJU B., GUPTA N. K.
- Date : 1985
- Languages : English
- Source: Indian J. Cryog. - vol. 10 - n. 3
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INDUSTRIAL-SCALE LIQUID HYDROGEN TRANSFER SYSTEM.
- Author(s) : KUSTERER H.
- Date : 1987/08/24
- Languages : English
- Source: Development in refrigeration, refrigeration for development. Proceedings of the XVIIth international Congress of Refrigeration.
- Formats : PDF
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