AUTOMATIC LIGHT AIRCRAFT READINESS MONITOR. VOLUME III. ADDENDUM - REINSTALLATION, PHASE II. TEST PROGRAM

Abstract

Discussions are presented on the installation procedures, calibration data, and results of tests on the modified Automatic Light Aircraft Readiness Monitor (ALARM) System Installation. The aircraft airframe was modified and new transmission and gear boxes were installed during the aircraft overhaul. In addition, the tail vibration sensor was relocated. The modified ALARM System virtually eliminates temperature drift, and the results of this phase compare favorably with the test program results.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1963
Accession Number
AD0414526

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Sensors

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Chemical Reactions
  • Circuit Breakers
  • Circuits
  • Detection
  • Detectors
  • Frequency
  • Government Procurement
  • Oil Filters
  • Plastic Explosives
  • Power Supplies
  • Relief Valves
  • Resistance
  • Tail Rotors
  • Test Beds
  • Test Equipment

Readers

  • Aerospace Test and Evaluation
  • Software Engineering