Abstract

Specifies single-degree-of-freedom spring-restrained rate gyro for (aircraft, missile, spacecraft) applications, to provide ((dc, ac) voltage outputs proportional to angular rate inputs up to _______ degrees per second, switch closure(s) at angular rates (exceeding, less than) ________ (+,-, ) ________ degrees per second).

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	Institute of Electrical & Electronics Engineers
Pages
ISBN