FLIGHT TEST WORKING GROUP. FLIGHT TEST REPORT ATLAS MISSILE 62D. (WS 107A-1)

Abstract

This report defines the flight performance of a guided missile. The primary purposes of this flight were to determine the performance of the re- entry vehicle, with principle emphasis on the operation of the simulated war-head, and to evaluate the guidance system accuracy. Detailed objectives are listed along with comments on the degree to which they were satisfied.

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Document Details

Document Type
Technical Report
Publication Date
Jun 29, 1960
Accession Number
AD0841975

Entities

People

  • D. D. Hammett
  • L. E. Kolderup
  • R. E. Payne
  • R. W. Taylor
  • V. K. Smith

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Altitude
  • Control Systems
  • Engines
  • Fuel Systems
  • High Pressure
  • Instrumentation
  • Load Cells
  • Measurement
  • Pressure Switches
  • Propulsion Systems
  • Range Safety
  • Recording Systems
  • Regulators
  • Rocket Engines
  • Rockets
  • Sustainer Engines
  • Telemetry

Readers

  • Aerospace Test and Evaluation
  • Library and Information Science