PRELIMINARY TEST PROCEDURES FOR TESTING XSM-65A MISSILE PROPULSION SYSTEM INSTALLATION 7-20001.

Abstract

This Test Procedure provides test equipment operating instructions required to perform post-installation operational acceptance tests of the Missile propulsion system. The test procedure is divided into two parts: (1) Integrated component operation test, (2) Propulsion system sequence operation test. Part 1 must be successfully completed before beginning Part 2, and the checkout operations must follow in the order given in this procedure. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 30, 1956
Accession Number
AD0829233

Entities

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Acceptance Tests
  • Instructions
  • Propulsion Systems
  • Sequences
  • Test Equipment

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation