Various theories [1,2] have been proposed for the pressure dependence of burning rate of composite propellants since a knowledge of this pressure dependence is vital for the design of a solid propellant rocket motor. Recently, Girdhar and Arora [3] have measured the burning rate of phenol-formaldehy
โฆ LIBER โฆ
Mechanism of Burning Rate Enhancement of Composite Solid Propellants by Ferric Oxide
โ Scribed by Chakravarthy, Satyanarayanan R.; Price, Edward W.; Sigman, Robert K.
- Book ID
- 120028939
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 1997
- Tongue
- English
- Weight
- 373 KB
- Volume
- 13
- Category
- Article
- ISSN
- 0748-4658
- DOI
- 10.2514/2.5208
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## Abstract One of the principal parameters associated with a solid propellant is its linear burning rate. Many attempts have been made in the past to determine theoretically the burning rates of solid propellants by the use of appropriate combustion models. The object of the present paper is to pr
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