Accession Number:

AD0605853

Title:

Total Impulse Measuring System for Solid Propellant Rocket Engine: Phase I Report

Descriptive Note:

Corporate Author:

ROCKETDYNE CANOGA PARK CA

Personal Author(s):

Report Date:

1963-06-01

Pagination or Media Count:

153.0

Abstract:

Discussion and results of three main considerations are presented 1 study and discussion of the use site and existing measurement system at EAFB, with recommendations for the installation of the Rocketdyne system 2 general and applied mathematical analyses of springmass total impulse measurement systems and 3 mechanical and electrical design of the Rocketdyne system to be constructed. Specific results of these separate but related program efforts are, respectively 1 concurrence with the general approach taken in the existing EAFB system, but disagreement with some specific design, installation, and operational features of the system 2 new and original mathematical analyses whose results justify the Rocketdyne approach to the measurement problem and 3 new and original mechanical and electrical component designs.

Subject Categories:

  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE