Dual-Mode Combustion Characteristic of a Self-Quenched Solid Propellant in a Rocket Motor
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3496
Reference17 articles.
1. Thrust magnitude control for a solid rocket by injection at the throat.
2. A solid-propellant rocket motor modulated by a fluidic vortex valve
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4. Development of Test Motors for Advanced Controllable Propellants
5. Status of army pintle technology for controllable thrust propulsion
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