Microwave Doppler Shift Technique for Determining Solid Propellant Transient Regression Rates
Author:
Affiliation:
1. Jet Propulsion Laboratory, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.62012
Reference31 articles.
1. Depressurization induced extinction of burning solid propellant.
2. A review of calculations for unsteady burning of a solid propellant.
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