Transient Burning of Solid Propellants
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/5.9781600865671.0599.0659
Reference168 articles.
1. A Simplified Model of Unstable Burning in Solid Propellants
2. Nonsteady burning phenomena of solid propellants - Theory and experiments.
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1. Evaluation of Dynamic Burn Rate from the Extinction Compliance of Solid Rocket Motors;Journal of Spacecraft and Rockets;2007-03
2. Non-Steady Burning Effect on Solid Rocket Motor Performance;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08
3. Transient Burning Characteristics of JA2 Propellant Using Experimentally Determined Zel'Dovich Map (Invited);39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26
4. Nonlinear Intrinsic Instability of Solid Propellant Combustion Including Gas-Phase Thermal Inertia;Combustion Science and Technology;2000-09
5. The effect of radiant heat feedback on the unsteady combustion of metalized propellants;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24
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