Flight Test Report Atlas Missile 17E 22 June 1961.

Abstract

The primary purposes of this flight were to determine missile system extended range capability, evaluate guidance system performance and accuracy, determine performance of the Mark 3 Mod 1B re-entry vehicle, and determine the performance of the arming and fuzing system. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 06, 1961
Accession Number
AD0843380

Entities

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy

Readers

  • Ballistic Missile Meteorology
  • Munitions and Ordnance Engineering
  • Software Engineering