Accession Number:

AD0755825

Title:

Non-Acoustic Combustion Instability of Composite Solid Propellants.

Descriptive Note:

Scientific rept.,

Corporate Author:

UTAH UNIV SALT LAKE CITY DEPT OF CHEMICAL ENGINEERING

Personal Author(s):

Report Date:

1972-12-29

Pagination or Media Count:

146.0

Abstract:

The non-acoustic but nevertheless oscillatory combustion of composite solid propellants was studied with burners in which L could be increased or decreased during the course of a firing. A modular theory is suggested, and simplified for application to the data generated. Low-frequency, low-amplitude oscillations not characteristic of the propellant only. Author

Subject Categories:

  • Combustion and Ignition
  • Solid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE