WS 107A-1 Flight Test Working Group Flight Test Report Atlas Missile 4 F, 23 November 1961, AMR Range Test Number 3751 Astronautics Test Number P1- 601-00-4

Abstract

The primary purposes of this flight were to obtain data on the re- entry vehicle impact location for the statistical determination of the CEP, to evaluate the ability of the MAPCHE System and procedures to check out a missile and place it in a first readiness condition, to evaluate the Sandia simulated warhead, to evaluate the Acoustica PU System, and to evaluate the Inertial Guidance System performance and accuracy. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Nov 30, 1961
Accession Number
AD0844821

Entities

People

  • E. V. Thatcher
  • F. W. Adkins
  • L. D. Solid
  • T. R. Carden
  • W. M. Caldwell

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Control Systems
  • Detectors
  • Fibers
  • Flash Point
  • Flight Control Systems
  • Frequency Shift
  • Ground Stations
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Inverters
  • Measurement
  • Pressurization
  • Propulsion Systems
  • Regulators
  • Telemetry Equipment
  • Transducers

Readers

  • Aerospace Test and Evaluation
  • Missile Defense Systems.

Technology Areas

  • Space