Z(WS 107A-1)ZFlight Test Working Group Flight Test Report Atlas Missile 8 E, 24 January 1961. AMR Range Test Number 3504 Convair Test Number P3-503-00-08.

Abstract

The primary objectives for the flight test included evaluation of the production version of the MA-3 rocket engine propulsion system and evaluation of the lot IV inertial guidance system. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 03, 1961
Accession Number
AD0843820

Entities

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Engineering
  • Engines
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Mechanical Engineering
  • Navigation
  • Navigational Equipment
  • Propulsion Systems
  • Rocket Engines
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation