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Superfluid Helium Tanker (SFHT) studyReplenishment of superfluid helium (SFHe) offers the potential of extending the on-orbit life of observatories, satellite instruments, sensors and laboratories which operate in the 2 K temperature regime. A reference set of resupply customers was identified as representing realistic helium servicing requirements and interfaces for the first 10 years of superfluid helium tanker (SFHT) operations. These included the Space Infrared Telescope Facility (SIRTF), the Advanced X-ray Astrophysics Facility (AXAF), the Particle Astrophysics Magnet Facility (Astromag), and the Microgravity and Materials Processing Sciences Facility (MMPS)/Critical Point Phenomena Facility (CPPF). A mixed-fleet approach to SFHT utilization was considered. The tanker permits servicing from the Shuttle cargo bay, in situ when attached to the OMV and carried to the user spacecraft, and as a depot at the Space Station. A SFHT Dewar ground servicing concept was developed which uses a dedicated ground cooling heat exchanger to convert all the liquid, after initial fill as normal fluid, to superfluid for launch. This concept permits the tanker to be filled to a near full condition, and then cooled without any loss of fluid. The final load condition can be saturated superfluid with any desired ullage volume, or the tank can be totally filed and pressurized. The SFHT Dewar and helium plumbing system design has sufficient component redundancy to meet fail-operational, fail-safe requirements, and is designed structurally to meet a 50 mission life usage requirement. Technology development recommendations were made for the selected SFHT concept, and a Program Plan and cost estimate prepared for a phase C/D program spanning 72 months from initiation through first launch in 1997.
Document ID
19890010811
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Eberhardt, Ralph N.
(Martin Marietta Aerospace Denver, CO, United States)
Dominick, Sam M.
(Martin Marietta Aerospace Denver, CO, United States)
Anderson, John E.
(Martin Marietta Aerospace Denver, CO, United States)
Gille, John P.
(Martin Marietta Aerospace Denver, CO, United States)
Martin, Tim A.
(Martin Marietta Aerospace Denver, CO, United States)
Marino, John S.
(Martin Marietta Aerospace Denver, CO, United States)
Paynter, Howard L.
(Martin Marietta Aerospace Denver, CO, United States)
Traill, R. Eric
(Martin Marietta Aerospace Denver, CO, United States)
Herzl, Alfred
(Martin Marietta Aerospace Denver, CO, United States)
Gotlib, Sam
(Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:172110
NASA-CR-172110
MCR-88-1402
Report Number: NAS 1.26:172110
Report Number: NASA-CR-172110
Report Number: MCR-88-1402
Accession Number
89N20182
Funding Number(s)
CONTRACT_GRANT: NAS9-17854
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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