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Feasibility study for the Cryogenic Orbital Nitrogen Experiment (CONE)An improved understanding of low gravity subcritical cryogenic fluid behavior is critical for the continued development of space based systems. Although early experimental programs provided some fundamental understanding of zero gravity cryogenic fluid behavior, more extensive flight data are required to design space based cryogenic liquid storage and transfer systems with confidence. As NASA's mission concepts evolve, the demand for optimized in-space cryogenic systems is increasing. Cryogenic Orbital Nitrogen Experiment (CONE) is an attached shuttle payload experiment designed to address major technological issues associated with on-orbit storage and supply of cryogenic liquids. During its 7 day mission, CONE will conduct experiments and technology demonstrations in active and passive pressure control, stratification and mixing, liquid delivery and expulsion efficiency, and pressurant bottle recharge. These experiments, conducted with liquid nitrogen as the test fluid, will substantially extend the existing low gravity fluid data base and will provide future system designers with vital performance data from an orbital environment.
Document ID
19950006821
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bell, R. S.
(Ball Corp. Boulder, CO, United States)
Crouch, M. A.
(Ball Corp. Boulder, CO, United States)
Hanna, G. J.
(Ball Corp. Boulder, CO, United States)
Cady, E. C.
(Ball Corp. Boulder, CO, United States)
Meserole, J. S.
(Ball Corp. Boulder, CO, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-187231
NAS 1.26:187231
Report Number: NASA-CR-187231
Report Number: NAS 1.26:187231
Accession Number
95N13234
Funding Number(s)
PROJECT: RTOP 593-21-21
CONTRACT_GRANT: NAS3-25054
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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