Control of pressure deflagration limits of composite solid propellants.
- 1 April 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (4) , 764-770
- https://doi.org/10.2514/3.4059
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- AN EXPERIMENTAL STUDY OF THE ALUMINUM ADDITIVE ROLE IN UNSTABLE COMBUSTION OF SOLID ROCKET PROPELLANTSPublished by Elsevier ,1963