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Dependence of density and burning rate of composite solid propellant on mixer size

✍ 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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πŸ“œ SIMILAR VOLUMES


Dependence of burning rate of composite
✍ R.P. Rastogi; Ram Raj Singh; Anand P. Rao πŸ“‚ Article πŸ“… 1982 πŸ› Elsevier Science 🌐 English βš– 164 KB

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

Burning Rate Evaluation of Composite Sol
✍ V. Swaminathan; M. Soosaimarian πŸ“‚ Article πŸ“… 1981 πŸ› John Wiley and Sons 🌐 English βš– 403 KB

## 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

Pressure dependence of burning rate of n
✍ H.L. Girdhar; A.J. Arora; G.N. Malik πŸ“‚ Article πŸ“… 1980 πŸ› Elsevier Science 🌐 English βš– 221 KB

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