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New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic SystemsThe Phoenix Air-Launched Small Missile (ALSM) flight testbed was conceived and is proposed to help address the lack of quick-turnaround and cost-effective hypersonic flight research capabilities. The Phoenix ALSM testbed results from utilization of the United States Navy Phoenix AIM-54 (Hughes Aircraft Company, now Raytheon Company, Waltham, Massachusetts) long-range, guided air-to-air missile and the National Aeronautics and Space Administration (NASA) Dryden Flight Research Center (Edwards, California) F-15B (McDonnell Douglas, now the Boeing Company, Chicago, Illinois) testbed airplane. The retirement of the Phoenix AIM-54 missiles from fleet operation has presented an opportunity for converting this flight asset into a new flight testbed. This cost-effective new platform will fill the gap in the test and evaluation of hypersonic systems for flight Mach numbers ranging from 3 to 5. Preliminary studies indicate that the Phoenix missile is a highly capable platform; when launched from a high-performance airplane, the guided Phoenix missile can boost research payloads to low hypersonic Mach numbers, enabling flight research in the supersonic-to-hypersonic transitional flight envelope. Experience gained from developing and operating the Phoenix ALSM testbed will assist the development and operation of future higher-performance ALSM flight testbeds as well as responsive microsatellite-small-payload air-launched space boosters.
Document ID
20070025193
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Bui, Trong T.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Lux, David P.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Stenger, Michael T.
(Naval Air Warfare Center China Lake, CA, United States)
Munson, Michael J.
(Naval Air Warfare Center China Lake, CA, United States)
Teate, George F.
(Science Applications International Corp. Edwards, CA, United States)
Date Acquired
August 23, 2013
Publication Date
August 1, 2007
Subject Category
Aeronautics (General)
Report/Patent Number
H-2634
NASA/TM-2007-214624
Distribution Limits
Public
Copyright
Public Use Permitted.
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