IEEE 292 1969
$47.67
IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros
Published By | Publication Date | Number of Pages |
IEEE | 1969 | 29 |
New IEEE Standard – Active. 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]. An errata is available at http://standards.ieee.org/findstds/errata/292-1969.pdf
PDF Catalog
PDF Pages | PDF Title |
---|---|
1 | Title Page |
2 | Participants |
3 | Introduction |
5 | CONTENTS |
7 | 1. Scope 2. Applicable Documents 2.1 Specifications 2.2 Standards |
8 | 2.3 Drawings 2.4 Bulletins 2.5 Other Publications 3. Requirements 3.1 Description 3.2 General Requirements |
9 | 3.3 Performance |
13 | 3.4 Mechanical |
14 | 3.5 Electrical |
16 | 3.6 Environmental |
19 | 3.7 Reliability 4. Quality Assurance Provisions 4.1 Classification of Tests 4.2 Acceptance Tests |
21 | 4.3 Qualification Tests 4.4 Reliability Tests |
23 | 4.5 Test Conditions and Equipment 4.6 Test Methods |
25 | 4.7 Test Data Submittal 5. Preparation For Delivery 6. Notes 6.1 Intended Use |
26 | 6.2 Ordering Data 6.3 Model Equation |