Burning Rate Control Factors in Solid Propellants
Quarterly technical summary rept. no. 7, 1 Jul-30 Sep 1960
PRINCETON UNIV NJ DEPT OF AERONAUTICAL ENGINEERING
Pagination or Media Count:
During the past quarter work under this contract has been directed primarily at 1 a continuation of the study of oxidizer particle size effects on burning rate, and 2 the transfer of operations to the newly constructed Solid Propellant Processing Building.
- Rocket Propellants