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Effect of pressure on the burning rate of composite propellants

✍ Scribed by Yu. S. Kichin; G. V. Lukashenya; N. N. Bakhman; A. F. Belyaev


Book ID
112393697
Publisher
SP MAIK Nauka/Interperiodica
Year
1970
Tongue
English
Weight
273 KB
Volume
6
Category
Article
ISSN
0010-5082

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πŸ“œ SIMILAR VOLUMES


Effect of pressure on burning rate of ph
✍ H.L. Girdhar; A.J. Arora πŸ“‚ Article πŸ“… 1979 πŸ› Elsevier Science 🌐 English βš– 220 KB

Burning rates of phenol-formaldehyde composite propellants based on NH4CI04, KCIO4, NaNOa, and KNO a oxidisers are measured under the pressure of nitrogen at 1-95 atm. The burning rate laws of the type (P[r) = (a + bP) and (P/r) = (a + bP21 a) are tested. It is revealed that the latter gives a super

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

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