Aerothermodynamic design feasibility of a generic planetary aerocapture/aeromaneuver vehicle
- 23 June 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Thermal protection system for the Galileo mission atmospheric entry probePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- A study of the aerothermal entry environmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Orders boost for building materialsIndustrial Management, 1978
- Viscous-shock-layer solutions with radiation and ablation injection for Jovian entryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Selection of a heat protection system for Venusian entryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- An approximate inviscid radiating flow-field analysis for sphere-cone Venusian entry vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Fully coupled nongray radiating gas flows with ablation product effects about planetary entry bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- On the Corridor and Associated Trajectory Accuracy for Entry of Manned Spacecraft into Planetary AtmospheresPublished by Springer Nature ,1960
- Supersonic Flow Around Blunt BodiesJournal of the Aerospace Sciences, 1958