FINAL REPORT 1960-1969.
COLUMBIA UNIV NEW YORK DEPT OF CIVIL ENGINEERING AND ENGINEERING MECHANICS
Pagination or Media Count:
A summary is given of research which emphasized a problems of material characterization that are relevant to real operating conditions of propellant grains and thus to their design b problems of analysis that reflect the observation that solid propellants of the high filler content used are quasi-homogeneous and quasi-continuous only at the very small strains that are far removed from conditions of incipient failure, as well as c problems arising from the desire to increase the operating burning pressures in the grain to an extent that would require the use of circumferential wire reinforcement.
- Solid Rocket Propellants