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

Abstract

Discussion and results of the two main considerations comprising the intermediate (Phase II) effort are presented: (1) fabrication and test of the component parts of the system prior to their inclusion in the system; and (2) assembly and test of the complete measurement system prior to its delivery to EAFB. Specific results of these separate but related program efforts are, respectively: (1) source inspections and tests, where needed, to determine compliance with Rocketdyne drawings and specifications, and (2) alignment measurements and detailed tests to determine that the overall system peerformance conformed to the contractual requirement of 0.1% accuracy.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1964
Accession Number
AD0606557

Entities

People

  • V. C. Plane

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Air Force
  • Air Force Facilities
  • Electrical Circuits
  • Fabrication
  • Jet Propulsion
  • Load Cells
  • Manufacturing
  • Measurement
  • Military Research
  • New Jersey
  • New York
  • North Carolina
  • Ordnance Laboratories
  • Power Supplies
  • Rocket Engines
  • Solid Propellants

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Rocket Propulsion.