✦ LIBER ✦

Dependence of burning rate of composite solid propellants on pressure

✍ Scribed by R.P. Rastogi; Ram Raj Singh; Anand P. Rao

Publisher: Elsevier Science
Year: 1982
Tongue: English
Weight: 164 KB
Volume: 45
Category: Article
ISSN: 0010-2180
DOI: 10.1016/0010-2180(82)90045-1

No coin nor oath required. For personal study only.

✦ Synopsis

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-formaldehyde composite propellants in the pressure range 1-95 atm using NH4C10 4 (AP), KC10 4, NaNO 3, and KNO 3 as oxidizers. The data were analyzed using the following equations: P

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