Accession Number:

AD0517835

Title:

Thermally Stable Burning Rate Accelerators

Descriptive Note:

Quarterly progress rept. no. 5, 1 Jun-31 Aug 1971

Corporate Author:

MORTON THIOKOL INC HUNTSVILLE AL HUNTSVILLE DIV

Personal Author(s):

Report Date:

1971-10-01

Pagination or Media Count:

28.0

Abstract:

Experiments have shown that the thermal stability of propellants is a direct function of UFAP and catalyst concentration. A new thermally stable catalyst has been synthesized and is undergoing preliminary evaluation. Indications are that fast burning propellants 2.5 insec at 1000 psi can be made using up to 30 UFAP and up to 3 catalyst.

Subject Categories:

  • Solid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE