Charge Geometry and Ballistic Parameters for Solid Propellant Rocket Motors
- 1 January 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Jet Propulsion
- Vol. 24 (1) , 16-21
- https://doi.org/10.2514/8.6440
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Theory of Steady Flow with Mass Addition Applied to Solid Propellant Rocket MotorsJournal of the American Rocket Society, 1953