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Water sprays in space retrieval operationsThe water spray technique (WST) for nullifying the angular momentum of a disabled spacecraft is examined. Such a despinning operation is necessary before a disabled spacecraft can be retrieved by the Space Shuttle. The WST involving the use of liquid sprays appears to be less complex and costly than other techniques proposed to despin a disabled vehicle. A series of experiments have been conducted to determine physical properties of water sprays exhausting into a vacuum. A computer model is built which together with the experimental results yields satellite despin performance parameters. The selection and retrieval of an actual disabled spacecraft is considered to demonstrate an application of the WST.
Document ID
19780040114
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Freesland, D. C.
(Pennsylvania State University University Park, Pa.; Martin Marietta Aerospace, Bethesda, Md., United States)
Date Acquired
August 9, 2013
Publication Date
February 1, 1978
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 78-329
Meeting Information
Meeting: Annual Meeting and Technical Display
Location: Washington, DC
Start Date: February 7, 1978
End Date: February 9, 1978
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
78A24023
Funding Number(s)
CONTRACT_GRANT: NSG-7078
Distribution Limits
Public
Copyright
Other

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