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Accession Number:

AD0835810

Title:

Combustion of Solid Propellants and Low Frequency Combustion Instability

Corporate Author:

NAVAL WEAPONS CENTER CHINA LAKE CA

Report Date:

1968-04-01

Abstract:

This semiannual report summarizes studies of ammonium perchlorate decomposition and deflagration, behavior of aluminum in the combustion zone of propellants, and oscillatory combustion of propellants in several types of experimental arrangements. Author

Descriptive Note:

Progress rept. 1 Apr-30 Sep 1967

Supplementary Note:

NASA Work Order No. 6030.

Pages:

0115

Descriptors:

COMBUSTION

SOLID ROCKET PROPELLANTS

ACOUSTIC IMPEDANCE

ADIABATIC GAS FLOW

ALUMINUM

AMMONIUM PERCHLORATE

BURNING RATE

COMPOSITE PROPELLANTS

DEFLAGRATION

ELECTRON MICROSCOPES

EROSIVE BURNING

MATHEMATICAL MODELS

PHOTOMICROGRAPHY

PROPELLANT BURN OUT

SOLID ROCKET OXIDIZERS

SOLID ROCKET PROPELLANT BINDERS

STABILITY

TEST METHODS

Identifiers:

COMBUSTION STABILITY

OSCILLATORY COMBUSTION

*SCANNING ELECTRON MICROSCOPES

SEM(SCANNING ELECTRON MICROSCOPE)

Subject Categories:

Combustion and Ignition

Solid Rocket Propellants

Communities Of Interest:

Weapons Technologies

Modernization Areas:

Directed Energy

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

2.58MB

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