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Development, Application, and Design Specifications of a Laser Doppler Particle Sensor for the Measurement of Particle Velocities in Two Phase Rocket Exhausts, Volume II.

Stanford University. Department of Aeronautics and Astronautics

出版	Defense Technical Information Center, 1968
URL	http://books.google.com.hk/books?id=zNIDAAAAIAAJ&hl=&source=gbs_api

註釋

The development of a prototype instrument to measure the velocity of particles in the exhaust of a solid rocket motor is described. This volume contains the design specifications for the prototype instrument used to obtain data on a five thousand (5,000) pound thrust rocket engine. (Author).