
Single-Degree-of-Freedom Spring-Restrained Rate Gyros
NORMA vydaná dňa 1.2.2008
Označenie normy: SAE AS1104
Dátum vydania normy: 1.2.2008
Krajina: Americká technická norma
Kategória: Technické normy SAE
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.
SUBJECT TAXONOMY: Avionics, Aircraft instruments, Aircraft displays, Flight control systems, Flight management systems, Interiors, Cabins, and Cockpits, Displays, Smoke detection, Instrument panels, Parts, Safety, Fire detection, Tests and Testing
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard