Accession Number:

AD0608451

Title:

EFFECT OF FIRING ROCKET SHELLS ON THE PERFORMANCE OF TURBOJET POWER PLANT,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1964-11-12

Pagination or Media Count:

10.0

Abstract:

The effects of firing rocket ammunition on the performance of axial flow turbojet engines are considered. The causes and effects of rocket launchings from airborne aircraft are discussed. Several recommendations for the prevention of these problems are given. The dynamic, thermal, and chemical effects on the performance of the power plant are described.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE