Flight Test Report Atlas Missile 16E, 24 March 1961.

Abstract

The primary purpose of the flight was to evaluate E series missile system performance at maximum R and D range. Other first order objectives included evaluation of Inertial Guidance System performance and accuracy, determination of warhead performance, arming and fuzing system performance, and missile system maximum range capability. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 06, 1961
Accession Number
AD0843410

Entities

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Navigation

Readers

  • Business Analytics
  • Munitions and Ordnance Engineering
  • Space Exploration and Orbital Mechanics.