Pegasus wing-glove experiment to document hypersonic crossflow transition - Measurement system and selected flight results-Reference-Cited by-同舟云学术

Pegasus wing-glove experiment to document hypersonic crossflow transition - Measurement system and selected flight results

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:38th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Bertelrud Arild¹,de la Tova Geva²,Hamory Philip³,Young Ronald³,Noffz Gregory³,Dodson Michael³,Graves Sharon⁴,Diamond John⁴,Bartlett James⁴,Noack Robert⁵,e al

Affiliation:

1. Analytical Services and Materials, Inc., Edwards, CA

2. Computer Sciences Corp., Edwards, CA

3. NASA, Flight Research Center, Edwards, CA

4. NASA, Langley Research Center, Hampton, VA

5. Wyle Labs., Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-505

Reference39 articles.

1. The first stage of the Pegasus@vehicle consists of a fuselage, a wing, and a wing/fuselage fillet. These parts were assembled and integrated with the secondand third stagesof the vehicle a short time (weeks) before launch. In order to meet the requirement for FX-I to be assembled independently from the rest of the vehicle, FX-1 hardware was limited to installation on or in the wing and the wing/fuselage fillet. With a wing and a fillet provided by OSC, NASA was able to mount the glove, fairing, and instrumentation and could check the functionality of the instrumentation without being tied directly to a particular launch. This task was completed during the fall of 1996.

2. The FX-1 wing and fillet was integrated with the rest of the vehicle at Vandenberg Air Force Base, California, during the summer of 1998 when a primary payload with a suitable trajectory and adequate weight margin was identified. Final instrumentation integration and calibrations were performed at this time. Final wing surface quality and geometry inspection documentation was performed there as well and and compared with previous inspections at NASA and at the OSC Chandler, Arizona, facility.

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3. Aerosciences, Aero-Propulsion and Flight Mechanics Technology Development for NASA's Next Generation Launch Technology Program;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15