Aerothermal heating predictions for Mars Microprobe
- 12 January 1998
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Mars Microprobe entry analysisPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- Prediction and validation of Mars Pathfinder hypersonic aerodynamic data basePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Aerodynamics of the Mars Microprobe entry vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Influence of sonic-line location on Mars Pathfinder Probe aerothermodynamicsJournal of Spacecraft and Rockets, 1996
- Mars Pathfinder six-degree-of-freedom entry analysisJournal of Spacecraft and Rockets, 1995
- Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center - Aerothermodynamic Facilities ComplexPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Aerothermodynamic methods for a Mars environmental survey Mars entryJournal of Spacecraft and Rockets, 1994
- Stagnation-point radiative heating relations for earth and Mars entriesJournal of Spacecraft and Rockets, 1991