Z(WS 107A-1)ZFlight Test Working Group Flight Test Report, ATLAS Missile 4E, 20 November 1960.

Abstract

This was the second flight test of the 'E' Series airframe and MA-3 propulsion system and provided for continued testing of the ARMA All Inertial Guidance System and for impact data for CEP determination. The results of these and other flight test objectives are presented, along with comments relative to the degree of satisfaction. Premature flight termination precluded satisfying many of the objectives. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 08, 1960
Accession Number
AD0842984

Entities

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Airframes
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Navigation
  • Propulsion Systems

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Systems Analysis and Design