WS 107A-1 Flight Test Working Group, Flight Test Report, Atlas Missile 32E

Abstract

The primary purposes of the flight were to obtain data for determining the performance of the Propellant Utilization System and to evaluate the Inertial Guidance System Performance.

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Document Details

Document Type
Technical Report
Publication Date
Nov 17, 1961
Accession Number
AD0843200

Entities

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Control Systems
  • Detectors
  • Flight Control Systems
  • Fuel Tanks
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Inverters
  • Measurement
  • Pressure Measurement
  • Pressure Regulators
  • Propellants
  • Propulsion Systems
  • Regulators
  • Telemetry
  • Test And Evaluation
  • Warning Systems

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation