Accession Number:

ADA179222

Title:

An Approach of Preventing Combustion Vibrations of Rocket Engine with Lateral Baffle,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1987-03-25

Pagination or Media Count:

26.0

Abstract:

In the process of developing the variable thrust rocket engine, combustion vibrations are encountered in the low end of the operating conditions. We used a lateral baffle to satisfactorily solve the problem. This paper mainly introduces the experimental results and qualitative analysis. The approach is novel. It can be used as a reference. Keywords rocket engines

Subject Categories:

  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE