WS 107-1 Flight Test Working Group, Flight Test Report, Atlas Missile 26E.

Abstract

The primary purposes of the flight were to obtain data for statistical determination of CEP, evaluate the performance of the Acoustica PU system and to determine re-entry vehicle structural capabilities at high angle re-entry conditions. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 08, 1961
Accession Number
AD0843112

Entities

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Control Systems
  • Detectors
  • Flash Point
  • Flight Control Systems
  • Fuel Pumps
  • Ground Stations
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Instrumentation
  • Inverters
  • Measurement
  • Pressure Regulators
  • Pressurization
  • Propulsion Systems
  • Regulators
  • Telemetry

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation