Effects of liquid burn rate catalysts on Rheological Properties of High-Energy Composite Propellants

Author:

Vuga Slobodan M.

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Reference12 articles.

1. “Study of the Possibility of Changing the Burning Rate in High-Energy Composite Rocket Propellant”, M. Sc. Study, School of Chemical Engineering, Belgrade, 1988, pp. 7-9

2. “Židkije i tverdije hemičeskije raketnije topliva”, Izdateljstvo Nauka, Moskva, 1978, pp. 62-73

3. U.S. Patent 4019933 (1977), Secretary of the U. S. Army, USA.

4. “Study of Metallocarboranes as Combustion Modifiers”, JANNAF Propulsion Meeting, CPIA Publication 340, 1981. pp. 253-287.

5. U.S. Patent 4352700 (1982), Secretary of the U.S. Army, USA.

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