WS-107A-1 Flight Test Working Group, Flight Test Report ATLAS missile 30E

Abstract

The primary purposes of the flight were to evaluate re-entry vehicle performance under conditions of extreme heating and to demonstrate the satisfactory performance of the airframe using a flattened trajectory. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Oct 12, 1961
Accession Number
AD0843132

Entities

People

  • J. R. Carden
  • K. E. Newton
  • L. D. Solid
  • T. W. Thatcher
  • W. H. Caldwell

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Actuators
  • Control Systems
  • Detectors
  • Flight Control Systems
  • Flow Rate
  • Fuel Tanks
  • Guidance
  • Ignition
  • Inertial Navigation
  • Inertial Navigation Systems
  • Inverters
  • Measurement
  • Propulsion Systems
  • Regulators
  • Rockets
  • Test And Evaluation
  • Transducers

Readers

  • Aerodynamics/Aeronautics.
  • Metallurgy
  • Software Engineering