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Background and Current Status of the Lifting Body ProgramThe lifting body concept was originally conceived by the Ames Research Center, and the design was developed over a period of years, from 1957 to 1964. By using a cone as a basic entry shape and modifying it to obtain lift and control, the M-2 shape evolved. In a cooperative venture with the NASA Ames Research Center to determine if a pilot could maneuver, flare, and land this class of vehicle, the Flight Research Center constructed a lightweight version of the lifting body, the M2-F1 vehicle. This vehicle was constructed during the fall of 1962 and spring of 1963 and extensively flight tested during the summer of 1963.

Because of the success of the M2-F1 flight program, the research program was extended to include vehicles that would be representative of mission weight and wing loading. Figure 1 shows the three vehicles in the present lifting body program. On the left is the X-24A vehicle, which evolved from the U. S. Air Force's SV-5 PRIME vehicle; in the center is the M2-F3 vehicle, which is a modified version of the M2-F2 vehicle; and on the right is the HL-10 vehicle, which evolved from work at the NASA Langley Research Center.
Document ID
19710000628
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
John G McTigue
(Flight Research Center Rosamond, California, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1970
Publication Information
Publication: Flight Test Results Pertaining to the Space Shuttlecraft
Publisher: National Aeronautics and Space Administration
Volume: NASA-TM-X-2101
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: NASA Symposium on Flight Test Results Pertaining to the Space Shuttlecraft
Location: Edwards, CA
Country: US
Start Date: June 30, 1970
Sponsors: Flight Research Center
Accession Number
71N10102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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