Confinement Removal before Ignition of Solid Propellant (CRISP)
Agency / Branch:
DOD / MDA
The objective of the proposed research and development effort is to demonstrate the feasibility of an innovative technology that will degrade or eliminate the ability of a rocket motor's composite case to contain pressure when subjected to Fast or Slow Cookoff thermal conditions. The project team also proposes a new hypothesis to explain the fragment throwing phenomenon. During the proposed project, the feasibility of this approach to hazard mitigation will be experimentally demonstrated.
Small Business Information at Submission:
12130 Rancho Road Adelanto, CA 92301
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