Ultrasonic measurements of solid propellant burning rates in nozzleless rocket motors
- 1 May 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 2 (3) , 215-222
- https://doi.org/10.2514/3.22872
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Prediction of solid propellant burning rates in nozzleless motorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Measurements and Model Validation for Composite Propellants Burning under Cross Flow of GasesAIAA Journal, 1980
- A model of the effects of pressure and crossflow velocity on composite propellant burning ratePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Microwave measurement of the solid propellant pressure-coupled response functionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Erosive Burning of Composite Solid Propellants: Experimental and Modeling StudiesJournal of Spacecraft and Rockets, 1979
- Reacting Turbulent Boundary-Layer Approach to Solid Propellant Erosive BurningAIAA Journal, 1978
- A Model of Erosive Burning of Composite PropellantsJournal of Spacecraft and Rockets, 1978
- Simulative Study on the Erosive Burning of Solid Rocket MotorsAIAA Journal, 1976
- Model Describing the Erosive Combustion and Velocity Response of Composite PropellantsAIAA Journal, 1975
- Flowfield in the Combustion Chamber of a Solid Propellant Rocket MotorAIAA Journal, 1974