Expansion of the scramjet ground test envelope of the hypulse facility

Space Plane and Hypersonic Systems and Technology Conference

Volumn , Issue , 1996, Pages

  Bakes, R J ^a   Castrogiovanni, A ^a   Calleja, J F ^a   Nucci, L ^a   Erdos, J I ^a  

^a GASL Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DYNAMICS; NASA; SPACECRAFT;

DYNAMIC PRESSURES; EXPANSION TUBES; HYPERSONIC NOZZLES; HYPERVELOCITIES; OPERATING MODES; REFLECTED SHOCKS; SCRAMJET TESTING; TEST CAPABILITY;

SHOCK TESTING;

EID: 84983161199     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

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2. Erdos, J., Calleja, J. and Tamagno, J., “Increases in the Hypervelocity Test Envelope of the HYPULSE Shock-Expansion Tube,” AIAA 94-2524, June 1994.
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12. Chinitz, W., Tamagno, J., Erdos, J., Singh, D. and Rogers, C.,”Premixed Shock Induced Combustion Studies in the HYPULSE Facility,” AIAA Paper No. 92-3427, 1992.
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