Accession Number:

ADB010173

Title:

Simulated Air Launch Environment, Volume 2. Aeroheat Data Summary

Descriptive Note:

Final rept. Sep 1972-May 1974

Corporate Author:

MORTON THIOKOL INC HUNTSVILLE AL HUNTSVILLE DIV

Personal Author(s):

Report Date:

1974-10-01

Pagination or Media Count:

321.0

Abstract:

A program was conducted in which the response and failure charactersitcs of solid propellant rocket motors when subjected to transient thermal conditions representing air launch operational environments were recorded and analyzed. Future Air Force mission profiles were used. The Maverick motor, AGM-65A, was used as a test bed on the program.

Subject Categories:

  • Fluid Mechanics
  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE