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Combustion of LOX with H2(sub g) under subcritical, critical, and supercritical conditions (Task 1) and experimental observation of dense spray and mixing of impinging jets (Task 2)The objective was to achieve a better understanding of the combustion processes of liquid oxygen and gaseous hydrogen under broad range of pressure covering subcritical, critical, and supercritical conditions. The scope of the experimental work falls into the following areas: (1) design of the overall experimental setup; (2) modification of an existing windowed high pressure chamber; (3) design of the LOX feeding system; (4) provision of the safety features in the test rig design; (5) LOX cleanliness requirements; (6) cold shock testing; (7) implementation of data acquisition systems; (8) preliminary tests for system checkout; (9) modification of LOX feeding system; and (10) evaporation tests. Progress in each area is discussed.
Document ID
19920010833
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kuo, K. K.
(Pennsylvania State Univ. University Park, PA, United States)
Hsieh, W. H.
(Pennsylvania State Univ. University Park, PA, United States)
Cheung, F. B.
(Pennsylvania State Univ. University Park, PA, United States)
Yang, A. S.
(Pennsylvania State Univ. University Park, PA, United States)
Brown, J. J.
(Pennsylvania State Univ. University Park, PA, United States)
Woodward, R. D.
(Pennsylvania State Univ. University Park, PA, United States)
Kline, M. C.
(Pennsylvania State Univ. University Park, PA, United States)
Burch, R. L.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 6, 2013
Publication Date
February 28, 1992
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
NASA-CR-190113
NAS 1.26:190113
Accession Number
92N20075
Funding Number(s)
CONTRACT_GRANT: NAG8-174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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