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Space Shuttle ice suppression system validation, volume 2The influence of nozzle size is dramatically illustrated in lab runs. It appears that increasing the size of the nozzle provides better coverage of ogive and mid-region of the external tank. It is interesting to note, however, that for the bottom region of the external tank, coverage seems to decrease with nozzle size. This can be explained if both the assymmetry of the lower set of nozzles and the blockage provided by the Orbiter aft-support structure are taken into account.
Document ID
19840009177
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Porteiro, J. L. F.
(Texas A&M Univ. College Station, TX, United States)
Norton, D. J.
(Texas A&M Univ. College Station, TX, United States)
Pollock, T. C.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Space Transportation
Report/Patent Number
NAS 1.26:171741
NASA-CR-171741
TEES-TR-4587-82-01-VOL-2
Report Number: NAS 1.26:171741
Report Number: NASA-CR-171741
Report Number: TEES-TR-4587-82-01-VOL-2
Accession Number
84N17245
Funding Number(s)
CONTRACT_GRANT: NAS9-16443
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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