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Cryogen acquisition in orbitOrbital cryogen acquisition is a definite requirement for engine restart and/or propellant transfer on all major future missions. The most promising methods, especially for large scale vehicles, are acquisition by linear acceleration and acquisition by capillary systems. Intermittent acceleration and propellant settling requires some state-of-the-art extension since it has not been attempted on a large scale cryogen vehicle. Capillary acquisition systems offer the advantages of reusability, passiveness, low weight, and mission flexibility. The major disadvantage is that of an undeveloped technology. The method does not lend itself to verification through ground testing.
Document ID
19720012301
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hastings, L. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 6, 2013
Publication Date
November 1, 1971
Publication Information
Publication: Cryog. Res. at MSFC: Res. Achievements Rev., Vol. 4, No. 2
Subject Category
Physics, General
Accession Number
72N19951
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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