Rocket Motor Igniter for Precision Centroid of Thrust.
Abstract
An igniter for use in a rocket having a predetermined spin rate during flight. The rocket includes a plurality of motors facing out from the body of the rocket and each motor is fired in a predetermined sequence. The igniter includes a squib for igniting fine black powder in the cavity of the igniter. The powder is packed in the cavity of the igniter with the density substantially like a cake. A cover member retains the powder in the cavity for a sufficient time to achieve fast ignition. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 19, 1980
- Accession Number
- ADD008204
Entities
People
- Nathan P. Williams
- Robert E. Betts
Organizations
- United States Army