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
The use of fractal for prediction of burning rate of composite solid propellants
β Scribed by Manouchehr Nikazar; Mohammad B. Bagherpour; Bahram Dabir
- Book ID
- 107431547
- Publisher
- Springer-Verlag
- Year
- 2000
- Tongue
- English
- Weight
- 241 KB
- Volume
- 9
- Category
- Article
- ISSN
- 1003-2169
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π SIMILAR VOLUMES
It is assumed thai combustion takes place in the turbulent boundary tay,'~ and that the turbuh,tlt ~lante condsts o/ distorted " [letnwl,'ts" but otheru,ts,, vet,tins on a otob'cular scah' the charact~,ristics o/a laminar l~atne. /| /tat-pb~t,' heat-tran,~/rr ~:orv, latton wah a /actor/or truttspira
## 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