Chemical Inhibitor for Solid Propellants.
Abstract
It is an object of the present invention to provide a method for inhibiting burning on at least a portion of the exposed surface of a specimen of solid rocket propellant during deflagration. Solid propellant test strands are inhibited, i.e., prevented from burning in an uncontrolled fashion, by coating the strands with a liquid composition containing a partially cured phenol-formaldehyde in a volatile solvent, then volatizing the solvent.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 18, 1986
- Accession Number
- ADD012582
Entities
People
- Janet L. Laird
Organizations
- United States Department of the Air Force