Accession Number:

AD0517602

Title:

Fast-Burning Rate/High Slope Propellant Technology Program

Descriptive Note:

Final rept. 1 May 70-22 Apr 71

Corporate Author:

AEROJET SOLID PROPULSION CO SACRAMENTO CA

Personal Author(s):

Report Date:

1971-09-01

Pagination or Media Count:

71.0

Abstract:

Two candidate propellant formulations, ANB-3394 and ANB-3395-1, were developed that satisfied all the technical goals. Additionally, these propellants were successfully test fired in small scale motors verifying propellant ballistic properties, excellent liner propellant bonds, and propellant processability adequate for good grains. Author

Subject Categories:

  • Solid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE