Standard

IEEE 292-1969

Nov 1968 Withdrawn

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Language English

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Abstract

New IEEE Standard - Inactive-Reserved. This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs up to______ degrees per second, a switch closure(s) at angular rates (exceeding,less than)______ (+,-,±)______ degrees per second].

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Standard from IEEE
Published: November 30 1968
Withdrawn: March 25 2021
Document type: IS
Pages
ISBN: 978-0-7381-0542-0

Publisher: IEEE
Distributor: IEEE
ICS: 49.090
National Committee: IEEE Aerospace and Electronic Systems Society / Gyro Accelerometer Panel

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Referred by: IEEE 1554-2005
Refers: IEEE 293-1969
Refers: Aerospace Industries Association, EETC Report No. 5 (Revision A), “Standard Gyro Terminology,” June 1965

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Abstract

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