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by David Shia
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1-D transient thermal modeling of an ablative material (MCC-1) exposed to a simulated convective Titan 4 launch environment
Thomas R. Reinarts
Development of processing techniques for advanced thermal protection materials
Guna S. Selvaduray
Supersonic torch facility for ablative testing
A. Chaboki
Guna Selvaduray
Postflight aerothermodynamic analysis of Pegasus[copyright] using computational fluid dynamic techniques
Gary D. Kuhn
Task 4 supporting technology
P. A. Hogenson
An analysis of ablation-shield requirements for manned reentry vehicles
Leonard Roberts
