Wind-tunnel preflight test program for aeroassist flight experiment
- 17 August 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Direct simulation of aerothermal loads for an aeroassist flight experiment vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- A computational study of the flowfield surrounding the Aeroassist Flight Experiment vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- The rationale for an aeroassist flight experimentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Nonequilibrium radiation during re-entry at 10 km/sPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- A comparison of computed and measured aerodynamic characteristics ofa proposed aeroassist flight experiment configurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Direct simulation of typical AOTV entry flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Systems analysis and technology development for the NASA Orbit Transfer VehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A review of aeroassisted orbit transferPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- System design concepts and requirements for aeroassisted orbital transfer vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982