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].
| SDO | IEEE: Institute of Electrical and Electronics Engineers |
| Document Number | 292 |
| Publication Date | Nov. 30, 1968 |
| Language | en - English |
| Page Count | 16 |
| Revision Level | |
| Supercedes | |
| Committee | Gyro Accelerometer Panel |