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SAE AS1104

69th Edition, October 2001

Complete Document

Single-Degree-of-Freedom Spring-Restrained Rate Gyros

Includes all amendments and changes through Reaffirmation Notice , February 2008

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Product Details:

  • Revision: 69th Edition, October 2001
  • Published Date: February 2008
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 20
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

This specification covers that gyroscopic instrument normally defined as a "subminiature rate gyro." The rate gyro, when subjected to an angular rate about its input axis, provides an AC output voltage proportional to the angular rate. The subminiature size category generally includes gyro instruments of one (1) inch diameter or less and three and one-half (3 1/2) inches length or less. This specification defines the requirements for a subminiature spring-restrained, single-degree-of-freedom rate gyro for aircraft, missile, and spacecraft applications.
AIA/NAS Aerospace Standards