Magnetic flow meter measurement of solid propellant pressure-coupled responses using an acoustic analysis
Author:
Affiliation:
1. ONERA, 92322 Chatillon, France
2. Pennsylvania State University, University Park, Pennsylvania 16802
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.24051
Reference6 articles.
1. Direct measurement of high frequency, solid propellant, pressure-coupled admittances
2. Ultrasonic measurements of solid propellant burning rates in nozzleless rocket motors
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