An over view of research into a low cost hypersonic research flight test capability to increase the amount of hypersonic flight data to help bridge the large developmental gap between ground testing/analysis and major flight demonstrator Xplanes is provided. The major objectives included: develop an air launched missile booster research testbed; accurately deliver research payloads through programmable guidance to hypersonic test conditions; low cost; a high flight rate minimum of two flights per year and utilize surplus air launched missiles and NASA aircraft.
Phoenix Missile Hypersonic Testbed (PMHT): Project Concept Overview
SAE Aerospace Control and Guidance Systems Committee Meeting #99 ; 2007 ; Boulder, CO, United States
2007-03-01
Conference paper
No indication
English
Design of the Phoenix Missile Hypersonic Testbed (PMHT)
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