Forebody TPS sizing with radiation and ablation for the Stardust Sample Return Capsule
- 23 June 1997
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 22 references indexed in Scilit:
- Approximate calculation of transport coefficients of Earth and Mars atmospheric dissociating gasesJournal of Thermophysics and Heat Transfer, 1996
- Comparison of coupled radiative flow solutions with Project Fire II flight dataJournal of Thermophysics and Heat Transfer, 1995
- Mars Pathfinder trajectory based heating and ablation calculationsJournal of Spacecraft and Rockets, 1995
- Hypersonic nonequilibrium Navier-Stokes solutions over an ablating graphite nosetipJournal of Spacecraft and Rockets, 1994
- Trajectory-based heating analysis for the European Space Agency/Rosetta earth return vehicleJournal of Spacecraft and Rockets, 1994
- Review of chemical-kinetic problems of future NASA missions. II - Mars entriesJournal of Thermophysics and Heat Transfer, 1994
- New technique for low-to-high altitude predictions of ablative hypersonic flowfieldsJournal of Spacecraft and Rockets, 1992
- Basic Governing Equations for the Flight Regimes of Aeroassisted Orbital Transfer VehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Gas-phase chemistry of re-entry.AIAA Journal, 1967
- Ionization Rate of Air behind High-Speed Shock WavesPhysics of Fluids, 1966