IEEE 1156.4 1997
$60.13
IEEE Standard for Environmental Specifications for Spaceborne Computer Modules
Published By | Publication Date | Number of Pages |
IEEE | 1997 | 37 |
New IEEE Standard – Inactive – Withdrawn. Fundamental information on minimum environmental withstand conditions for space electronics is provided. The intent is to achieve uniformity and reproducibility in the test conditions for all spaceborne computer modules that may make up larger systems and are purported to have a rated environmental performance level. The specifications pertain to both the natural and artificial environments to which spaceborne computer modules may be exposed. These conditions include, but are not limited to, thermal, mechanical, electrical, and radiation stresses.
PDF Catalog
PDF Pages | PDF Title |
---|---|
1 | Title Page |
3 | Introduction Participants |
5 | CONTENTS |
7 | 1. Overview 1.1 Background |
8 | 1.2 Scope 1.3 Purpose 2. References 3. Definitions 3.1 Special word usage |
9 | 3.2 Other definitions 4. Parameters and performance 4.1 Parameter categories |
10 | 4.2 Performance levels 4.3 Performance level examples |
11 | 5. Test approach 5.1 Performance level qualification 5.2 Test duration 5.3 Initial and final measurements |
12 | 5.4 Qualification testing 5.5 Acceptance testing 6. Test requirements 6.1 Nonoperating conditions |
13 | 6.2 Operating conditions |
22 | 7. Test procedures 7.1 Qualification test procedures |
27 | Annex A Radiation environments |
33 | Annex B Nuclear weapons effects |
34 | Annex C Radiation effects on microelectronics |
36 | Annex D Radiation hardness assurance |
37 | Annex E Bibliography |