Aerothermal Postflight Analysis of the Sharp Edge Flight Experiment-II

The aerothermal instrumentation of the Sharp Edge Hypersonic Flight Experiment SHEFEX-II, which was launched from Andøya Rocket Range on top of a two-stage rocket configuration, provided very useful flight data. Complementary to the pressure data, heat flux rate and surface temperature were measured...

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Bibliographic Details
Published in:Journal of Spacecraft and Rockets
Main Authors: Gülhan, A., Neeb, Dominik, Thiele, Thomas, Siebe, Frank
Other Authors: Edquist, K. T.
Format: Article in Journal/Newspaper
Language:unknown
Published: American Institute of Aeronautics and Astronautics (AIAA) 2015
Subjects:
Online Access:https://elib.dlr.de/101591/
http://arc.aiaa.org/doi/abs/10.2514/1.A33275