Withdrawn
, Confirmed
Standard
Most Recent
IEEE 292:1969 (R2010)
IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros
Summary
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].
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].
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].
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].
Notes
Inactive-Reserved
Technical characteristics
No products.
Previous versions
30/11/1968
Withdrawn
, Confirmed
Most Recent