Design of Graphite Nosetips for Ballistic Re-Entry
- 1 September 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 10 (9) , 592-598
- https://doi.org/10.2514/3.61931
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Carbon-carbon 3-D orthogonal material behaviorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- The ablation of graphitic materials in the sublimation regimePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Recent graphite nosetip developmentsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Hyperthermal ablation performance of carbon- carbon compositesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Axisymmetric ablation with shape changes and internal heat conductionAIAA Journal, 1970
- Shape and surface roughness effects on turbulent nosetip ablationAIAA Journal, 1970
- THERMODYNAMIC PERFORMANCE OF CARBON IN HYPERTHERMAL ENVIRONMENTSPublished by Elsevier ,1969