QUALIFICATION TEST OF LMSC 1348399 FAILURE SENSOR, TYPE 3.

Abstract

The purpose of this test was to determine the effects of vibration, shock, acceleration, temperature-altitude, and temperature-humidity on the performance capability of the Failure Sensor. A performance test was conducted subsequent to each environment. The specimen was operational only during temperature-altitude. The specimen meet all requirements of the test procedure.

Document Details

Document Type
Technical Report
Publication Date
Sep 28, 1965
Accession Number
AD0801533

Entities

People

  • W. G. Moore

Organizations

  • Lockheed Martin Missiles and Space

Tags

DTIC Thesaurus Topics

  • Altitude
  • Biological Phenomena
  • Climate
  • Ecological And Environmental Phenomena
  • Environment
  • Humidity
  • Motion
  • Performance Tests
  • Qualifications
  • Vibration
  • Wet Bulb Temperature

Fields of Study

  • Engineering

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Software Engineering