Ablation of refrasil-phenolic nozzle inserts in solid propellant exhausts
- 1 May 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 2 (3) , 337-344
- https://doi.org/10.2514/3.28181
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- THEORY FOR THE ABLATION OF FIBERGLAS-REINFORCED PHENOLIC RESINAIAA Journal, 1963
- Analysis of Convective Heat Transfer in Rocket NozzlesARS Journal, 1961
- Ablation Mechanisms in Plastics With Inorganic ReinforcementARS Journal, 1961
- Velocity Lag of Particles in Linearly Accelerated Combustion GasesJournal of Jet Propulsion, 1955