Accession Number:
AD0423152
Title:
THE CHARACTERIZATION OF SOLID ROCKET PROPELLANTS BY DIFFERENTIAL THERMAL ANALYSIS,
Descriptive Note:
Corporate Author:
ARMY MISSILE COMMAND REDSTONE ARSENAL ALA ARMY PROPULSION LAB AND CENTER
Personal Author(s):
Report Date:
1963-09-17
Pagination or Media Count:
26.0
Abstract:
Differential thermal analysis DTA is described for the characterization of solid rocket propellants. Variables, such as sample size and heating rates, are discussed. A DTA apparatus is tested and recommended for routine characterizations of a wide variety of propellant materials. The need is apparent for the standardization of DTA apparatus. Author