PROJECT SOPHY SOLID PROPELLANT HAZARDS PROGRAM
Abstract
A final appraisal of the RUBY computer program is presented, which concludes that the program is unsuitable for predicting the detonation properties of typical solid composite propellant. Analysis of the parameter c of the Aerojet detonation model continues. Mean critical diameters of two batches of RDX-adulterated AP-PBAN propellants are compared statistically. The critical- diameter test of a 72-in. dia. sample of unadulterated AP-PBAN propellant resulted in a sustained detonation. The results of the test are presented.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 28, 1966
- Accession Number
- AD0484737
Entities
People
- O. R. Irwin
- R. B. Elwell
- R. W. Vail
Organizations
- Aerojet Rocketdyne Holdings