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Mechanical properties of solid rocket propellants

1996
ABSTRACT MECHANICAL PROPERTIES OF SOLD) ROCKET PROPELLANTS Göçmez, Ahmet M.S., Department of Chemical Engineering Supervisor: Prof.Dr. Ülkü Yılmazer Co-Supervisor: Prof.Dr. Saim Özkar September 1996, 81 pages The oxidizer (ammonium perchlorate) content of HTPB-based composite solid propellants was increased to improve the performance of solid rocket ...
openaire   +2 more sources

The Thermal Theory of Ignition of Solid Propellants

The Journal of Physical and Colloid Chemistry, 1950
J H, FRAZER, B L, HICKS
openaire   +2 more sources

Performance calculations for solid propellant ramrockets

32nd Joint Propulsion Conference and Exhibit, 1996
Pein, R., Krishnan, S. (1)
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Differences of thermal decomposition behaviors and combustion properties between CL-20-based propellants and HMX-based solid propellants

Journal of Thermal Analysis and Calorimetry, 2019
Shuiping Zhou   +4 more
semanticscholar   +1 more source

Toxicity Problems with Solid Missile Propellants

Archives of Environmental Health: An International Journal, 1961
C W, KRAUL, R H, DUGUID
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