Accession Number:

AD0420602

Title:

One Method of Determining the Criterion of Operational Stability of a Liquid-Propellant Rocket Engine

Descriptive Note:

[Technical Report, Technical Report]

Corporate Author:

AIR FORCE SYSTEMS COMMAND WRIGHT-PATTERSON AFB OH

Personal Author(s):

• Zamuruyev, G. I.

Report Date:

1963-08-16

Pagination or Media Count:

31

Abstract:

Presented is a method of determining the criterion of operational stability of a liquid-propellant rocket engine.

Descriptors:

Subject Categories:

• Rocket Engines

Distribution Statement:

[A, Approved For Public Release]