Piloted simulator studies of the HL-20 Lifting BodyAn overview is presented of the concept, design and development of the NASA Langley Lifting Body, and the flight simulator studies that have been performed. Attention is given to the aerodynamic shape of the HL-20, vehicle and simulator/cockpit description, and evolution of the HL-20 aerodynamic model. The flight simulation studies have demonstrated the HL-20 to be a viable design for accomplishing precise, unpowered, horizontal landings.
Document ID
19920057409
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rivers, Robert A. (NASA Langley Research Center Hampton, VA, United States)
Jackson, E. B. (NASA Langley Research Center Hampton, VA, United States)
Ragsdale, W. A. (Unisys Corp. Detroit, MI, United States)