DESCRIPTION OF A 7-INCH-DIAMETER UNCURED SOLID PROPELLANT ROCKET MOTOR MALFUNCTION.
Abstract
A small, uncured solid propellant test motor overpressured destructively during a qualification firing. The test objectives were to evaluate the propellant ballistic properties and to determine the feasibility of a free-standing paper phenolic insulation tube. Possible failure modes and causes are proposed and discussed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1968
- Accession Number
- AD0841966
Entities
People
- John R. Ellison
Organizations
- Air Force Research Laboratory