Development, Application, and Design Specifications of a Laser-Doppler Particle Sensor for the Measurement of Particle Velocities in Two-Phase Rocket Exhausts. Volume II.
Abstract
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1968
- Accession Number
- AD0845191
Entities
People
- Barclay J. Tullis
- Howard L. Morse
- Howard S. Seifert
- Wayne R. Babcock
Organizations
- Stanford University