Strand size and low-pressure deflagration limit in a composite propellant
- 1 May 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (5) , 864-866
- https://doi.org/10.2514/3.5779
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- The theory of burning of solid and liquid propellantsCombustion and Flame, 1960