QUALIFICATION TEST OF THE PITCH REACTION WHEEL ELECTRONICS, LMSD P/N 1315322,

Abstract

The Pitch Reaction Wheel Electronics is a sealed unit used in the satellite attitude control system. This report describes the test conducted for qualification of the pitch reaction wheel in various controlled electrical and physical environments.

Document Details

Document Type
Technical Report
Publication Date
May 08, 1961
Accession Number
AD0801107

Entities

People

  • J. P. Wiley
  • W. F. Mcdonell

Organizations

  • Lockheed Martin Missiles and Space

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Traffic Control Systems
  • Artificial Satellites
  • Attitude Control Systems
  • Control Systems
  • Electronics
  • Entry Control Systems
  • Environment
  • Flight Control Systems
  • Qualifications
  • Satellite Attitude Control
  • Satellite Orientation

Fields of Study

  • Engineering

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Test and Evaluation
  • Exercise and Sports Science.

Technology Areas

  • Microelectronics
  • Space
  • Space - Spacecraft Maneuvers