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
No indication
English
Online Contents | 1996
|NTIS | 1967
|High Strain-Rate Impact Ignition of Rocket Propellants
British Library Conference Proceedings | 1993
|