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Liquid Hydrogen Microgravity Flight Experiment Concept

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Advances in Cryogenic Engineering

Part of the book series: Advances in Cryogenic Engineering ((ACRE,volume 39))

Abstract

A technological breakthrough is needed in the area of zero-g hydrogen management capabilities to enable future NASA, Air Force, and commercial missions, which all depend on liquid hydrogen and oxygen, the highest energy liquid rocket propellants available. In terms of liquid hydrogen fluid transfer, slosh, storing and dumping, there has been very little or no flight technology demonstrations applicable to the current needs of NASA, the Air Force, and the commercial sector. In order to enable the efficient, reduced risk, and low cost missions necessary in today’s austere space program environment, it is crucial to provide the fluid technologies needed for current and advanced upper stages and future hydrogen-fueled vehicles. This technology will allow launch systems to provide greater payloads at a reduced cost through more efficient zero and low-gravity handling of cryogenic propellant liquids in launch vehicle tanks. A design concept for a four-tank arrangement, packaged to perform the major objectives of subcritical liquid hydrogen handling experiments in zero-g, is presented, and is capable of fitting into several candidate NASA carriers. The baselined COMET (Commercial Experiment Transporter), launched on the Conestoga launch vehicle, would function as a free-flying experiment for at least three months at a microgravity environment of 10-5 g’s or lower.1 The completion of this experimental program will advance the state-of-the-art in the technology areas of cryogenic fluid transfer, storage, and slosh control dynamics in microgravity environments.

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References

  1. COMET Customers Operational Guide, Center for Space Transportation and Applied Research, Tullahoma, Tennessee (1992).

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  2. M.W. Liggett, F.O. Bennett, C.N. Torre and M.J. Sedillo “Long-Term Cryogenic Storage Facility Systems Study: Phase I - III Executive Summary” Report, prepared under contract number NAS8-36612 for NASA-Marshall Space Flight Center, Report number GDSS-CRAD-99-004 (1988)

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  3. J.R. Schuster, E. J. Russ, and J. P. Wachter. “Cryogenic On-Orbit Liquid Depot Storage, Acquisition, and Transfer Satellite (COLD-SAT) Feasibility Study Final Report”, prepared under contract number NAS3-25062 for NASA-Lewis Research Center, NASA Contractor Report 185249 (1990).

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  4. M.W. Liggett, “Space-Based LH2 Propellant Storage: Subscale Ground Testing Results” Cryogenics 33, 4: 438–442 (1993).

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  5. R.J. Hung, C.C. Lee, and F.W. Leslie, “Slosh Wave Excitation In A Partially Filled Rotating Tank Due To Gravity Jitters In A Microgravity Environment”, Acta Astronautica, Vol. 25, No. 8/9, pp. 523–551, 1991. Great Britain.

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  6. M.W. Liggett, W.J. Taylor, M.D. Walter, and G.E. Williams. “The Cryogenic On-Orbit Liquid Analytical Tool (COOLANT): a Program for Evaluating the Thermodynamic Performance of Orbital Cryogen Storage Facilities” Proc 29th AIAA Aerospace Sciences Meeting Reno, Nevada, (1991).

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© 1994 Springer Science+Business Media New York

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Liggett, M.W., Karr, G.R. (1994). Liquid Hydrogen Microgravity Flight Experiment Concept. In: Kittel, P. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 39. Springer, Boston, MA. https://doi.org/10.1007/978-1-4615-2522-6_24

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  • DOI: https://doi.org/10.1007/978-1-4615-2522-6_24

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4613-6074-2

  • Online ISBN: 978-1-4615-2522-6

  • eBook Packages: Springer Book Archive

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