Calculation of transient thermal stresses in solid rocket propellants

Author:

COST T.1

Affiliation:

1. Alabama, University, University, AL

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. 'ufferd,W.L., Lindsey,O., Parmeter, R., andSchapery,R.A. "Predictive Techniques for Failure Mechanisms in Solid Rocket Motors," U.S. Air ForcRocket PropulsionLaboratory, Edwards AirForceBase,Calif.,AFRPLTR-79-87,Jan.1980.

2. artinin, D.L.Jr. "An IntrinsicTime Shift Function for Solid Propellants,"U.S. ArmyMissileCommand,RedstoneArsenal,Ah., RK-81-0,June 1981. solidrocketmotorsunderthermaltoragecondition^.^

3. 3wanson,S.R., Chxistcnscn,L.W., and Chrbtensen,J. "A Nodbar Constitutive Law for High Eloq@on Propellant," JANNAF Structures and Mechanical Behavior Mbotlw Bulletin, CPfAPub.331,Dcc.1980.

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