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Effect of Specific Surface Area of Aluminum on Composite Solid Propellant Burning

โœ Scribed by Verma, Sumit; Ramakrishna, P. A.

Book ID
120447212
Publisher
American Institute of Aeronautics and Astronautics
Year
2013
Tongue
English
Weight
369 KB
Volume
29
Category
Article
ISSN
0748-4658

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๐Ÿ“œ SIMILAR VOLUMES

Dependence of burning rate of composite
Dependence of burning rate of composite solid propellants on pressure
โœ R.P. Rastogi; Ram Raj Singh; Anand P. Rao ๐Ÿ“‚ Article ๐Ÿ“… 1982 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 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