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
Dependence of density and burning rate of composite solid propellant on mixer size
β Scribed by Verma, Sumit; Ramakrishna, P.A.
- Book ID
- 120796669
- Publisher
- Elsevier Science
- Year
- 2014
- Tongue
- English
- Weight
- 729 KB
- Volume
- 93
- Category
- Article
- ISSN
- 0094-5765
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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
Polymers of o-, m-, and p-nitrophenols with formaldehyde were used as fuel binders in composite propellants based on NH 4C]O 4 and KCIO 4 oxidizers. A study of the burning rate in nitrogen has revealed the occurrence of a breakpoint at about 3-5 atm in the burning rate-pressure curves of all six typ