Ablation of Galileo Probe heat-shield models in a ballistic range
- 1 February 1985
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 23 (2), 301-308
- https://doi.org/10.2514/3.8910
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Injection-induced turbulence in stagnation-point boundary layersAIAA Journal, 1984
- Stagnation-point ablation of carbonaceous flat disks. II ExperimentAIAA Journal, 1983
- Stagnation-point ablation of carbonaceous flat disks. I TheoryAIAA Journal, 1983
- Calculation of radiation from argon shock layersJournal of Quantitative Spectroscopy and Radiative Transfer, 1982
- Spallation of the Galileo probe heat shieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Galileo probe forebody flowfield predictions during Jupiter entryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Galileo probe forebody thermal protection - Benchmark heating environment calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- An evaluation of computer codes for simulating the Galileo Probe aerothermal entry environmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Correlation of Nosetip Boundary-Layer Transition Data Measured in Ballistics-Range ExperimentsAIAA Journal, 1981
- Development of an Aeroballistic Range Capability for Testing Re-Entry MaterialsJournal of Spacecraft and Rockets, 1975