TEST AND EVALUATION OF AQM-37A

Abstract

The following conclusions are made in corresponding order of the test objectives: (a) Because the target did not maintain level flight, there was no test to determine the target low altitude, level flight profile after being launched at 2,000 feet pressure altitude at a speed of 0.6 Mach indicated. (b) The target separation characteristics from the A-4B aircraft in a low altitude environment appear to be satisfactory.

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Document Details

Document Type
Technical Report
Publication Date
Feb 13, 1964
Accession Number
AD0430723

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Altitude
  • C Band
  • Cameras
  • Captive Flight
  • Control Systems
  • Environment
  • Flight
  • Instrumentation
  • Level Flight
  • Low Altitude
  • Photography
  • Space Operations
  • Test And Evaluation
  • Theodolites

Readers

  • Aviation Science / Aeronautics.
  • Brain and Cognitive Science; Experimental Psychology; Cognitive Neuroscience