Ablative nose shape change effects on re-entry vehicle aerodynamic performance
- 16 August 1972
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Effect on Slender Vehicle Dynamics of Change from Spherical to Conical Nose BluntnessJournal of Spacecraft and Rockets, 1972
- Conical nose shape effects on drag and static stability at Mach 10.Journal of Spacecraft and Rockets, 1972
- Influence of Asymmetric Transition on Re-Entry Vehicle CharacteristicsJournal of Spacecraft and Rockets, 1971
- A time dependent solution for the blunt body flow of a chemically reacting gas mixturePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Effect of boundary-layer transition on vehicle dynamicsJournal of Spacecraft and Rockets, 1969