Experimental and predicted aerodynamic characteristics of a proposedAssured Crew Return Vehicle (ACRV) lifting-body configuration at Mach 6 and 10
- 18 June 1990
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- A code calibration program in support of the Aeroassist Flight ExperimentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Ascent, abort, and entry capability assessment of a Space Station rescue and personnel/logistics vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- A computational study of the flowfield surrounding the Aeroassist Flight Experiment vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Langley hypersonic facilities complex - Description and applicationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Experimental aerodynamic coefficients on a Shuttle-like vehicle at Mach 6 and 10 and comparison to predictionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985