The igniter composition for a solid rocket propellant consists essentially of powdered iron of a major amount by weight and potassium perchlorate.
Gasless Ignition Composition for Solid Rocket Propellants
1964
1 pages
Report
Keine Angabe
Englisch
Online Contents | 1996
|NTIS | 1967
|Ignition! : an informal history of liquid rocket propellants
TIBKAT | 1997
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