WS 107A-1 Flight Test Working Group. Flight Test Report, Atlas Missile 8F

Abstract

The purposes of the flight were to obtain data for statistical determination of CEP, evaluate the PU System, investigate the boattail heating and staging problems, evaluate the inertial guidance system performance, the re-entry vehicle performance and the performance of the arming and fuzing system. (Author)

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Oct 02, 1962
Accession Number
AD0861789

Entities

People

  • E. W. Thatcher
  • J. R. Carden
  • M. J. Swing
  • O. M. Henriksen
  • W. H. Caldwell

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Energy and Power Technologies
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Check Valves
  • Control Systems
  • Detectors
  • Flight Control Systems
  • Fuel Tanks
  • Guidance
  • Guidance Computers
  • Ignition
  • Inertial Navigation
  • Inertial Navigation Systems
  • Inverters
  • Measurement
  • Power Supplies
  • Pressure Measurement
  • Pressurization
  • Propulsion Systems
  • Regulators

Readers

  • Aerodynamics/Aeronautics.
  • Civilian Systems Systems Program Capability Development and Upgrade Support Activity Expense and Pay Management.
  • Inertial Navigation Systems.