NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Phoenix Missile Hypersonic Testbed (PMHT): Project Concept OverviewAn 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.
Document ID
20070014861
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Jones, Thomas P.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 23, 2013
Publication Date
March 1, 2007
Subject Category
Aerodynamics
Meeting Information
Meeting: SAE Aerospace Control and Guidance Systems Committee Meeting #99
Location: Boulder, CO
Country: United States
Start Date: February 28, 2007
End Date: March 2, 2007
Sponsors: Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available