COMBUSTION OF SOLID PROPELLANTS AT HIGH PRESSURES - A SURVEY
ROHM AND HAAS CO HUNTSVILLE AL
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The classified literature dealing with deflagration characteristics of solid propellants at pressures exceeding 2000 psia was screened. References from 1947 through 1964 on pure oxidizers and inert-binder composite propellants were assembled into an annotated bibliography.
- Solid Rocket Propellants