Lifting bodies (Aeronautics)--Flight testing
URI(s)
Components
Flight testing 
Broader Terms
Closely Matching Concepts from Other Schemes
Sources
found: Work cat.: Strutz, L.W. Flight-determined derivatives and dynamic characteristics for the HL-10 lifting body vehicle at subsonic and transonic Mach numbers, 1972:p. 9 (Test procedures. The HL-10 vehicle was carried aloft under the wing of a B-52 airplane and launched at an altitude of approximately 13,716 meters (45,000 feet) and a Mach number of approximately 0.7)
Instance Of
Scheme Membership(s)
Collection Membership(s)
Change Notes
2008-06-05: new
2008-06-06: revised
Alternate Formats
