Flight data analysis of the HyShot 2 scramjet flight experiment

Smart, M. K., Hass, N. E. and Paull, A. (2006) Flight data analysis of the HyShot 2 scramjet flight experiment. AIAA Journal, 44 10: 2366-2375. doi:10.2514/1.20661


Author Smart, M. K.
Hass, N. E.
Paull, A.
Title Flight data analysis of the HyShot 2 scramjet flight experiment
Journal name AIAA Journal   Check publisher's open access policy
ISSN 0001-1452
Publication date 2006-01-01
Sub-type Article (original research)
DOI 10.2514/1.20661
Volume 44
Issue 10
Start page 2366
End page 2375
Total pages 10
Editor Elaine S. Oran
Place of publication Reston
Publisher Amer Inst Aeronaut Astronaut
Language eng
Subject C1
290299 Aerospace Engineering not elsewhere classified
690302 Space transport
090107 Hypersonic Propulsion and Hypersonic Aerodynamics
Abstract The development of scramjet propulsion for alternative launch and payload delivery capabilities has been composed largely of ground experiments for the last 40 years. With the goal of validating the use of short duration ground test facilities, a ballistic reentry vehicle experiment called HyShot was devised to achieve supersonic combustion in flight above Mach 7.5. It consisted of a double wedge intake and two back-to-back constant area combustors; one supplied with hydrogen fuel at an equivalence ratio of 0.34 and the other unfueled. Of the two flights conducted, HyShot 1 failed to reach the desired altitude due to booster failure, whereas HyShot 2 successfully accomplished both the desired trajectory and satisfactory scramjet operation. Postflight data analysis of HyShot 2 confirmed the presence of supersonic combustion during the approximately 3 s test window at altitudes between 35 and 29 km. Reasonable correlation between flight and some preflight shock tunnel tests was observed.
Keyword Engineering
Aerospace
Q-Index Code C1

 
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Created: Wed, 15 Aug 2007, 18:46:15 EST