Accession Number:

AD0415401

Title:

INVESTIGATION OF ATLAS F-SERIES FLAME DEFLECTOR PRESSURE PULSE

Descriptive Note:

Corporate Author:

ROCKETDYNE CANOGA PARK CA

Personal Author(s):

Report Date:

1963-08-15

Pagination or Media Count:

65.0

Abstract:

Presented are the results of a test program to determine the effects of the pressure pulse that is generated in the flame deflector during initial thrust buildup of the Atlas MA-3 booster engine.

Subject Categories:

  • Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE