Combustion of Nitramine Propellants,
Abstract
The composite solid propellant combustion model of Beckstead, Derr and Price is modified to describe the combustion of Nitramine propellants. Modifications are based upon experimental observations of the combustion characteristics of hydrocarbon binder propellants containing cyclotetramethylenetetranitramine (HMX).
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1975
- Accession Number
- ADA004815
Entities
People
- Channon F. Price
- Norman S. Cohen
Organizations
- Lockheed Propulsion Company