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SMC-S-008
ELECTROMAGNETIC COMPATABILITY REQUIREMENTS FOR SPACE EQUIPMENT AND SYSTEMS
Year: 2008
Abstract: Purpose
The purpose of this document is to minimize risk to space programs in the area of electromagnetic compatibility (EMC).
Application
Document Applicability
This document is applicable to launch and space vehicles, their units and subsystems, plus the associated ground, airborne or spaceborne operational and support elements of the space system. This document does not apply to the facilities which house ground system segments of space systems (see MIL-STD-1542), nor does it apply to printed wiring board assemblies or individual microcircuits.
Requirement Applicability
The primary Requirements (e.g., 4.1, 6.05, 7.7), subrequirements (e.g., 4.2c2, 6.10c3, 7.1c1), verification methods (e.g., 4.3d1, 6.14d2, 7.7d) and tailoring (e.g., 4.1e1, 6.03e, 7.3e3) given in Sections 4 to 7 of this document are applicable in accordance with Table 1.2.2-1. They are also portion marked in the text in accordance with the explanation at the beginning of Table 1.2.2-1. All paragraphs under a primary Requirement have the same applicability as given at the primary Requirement title, unless otherwise marked.
The purpose of this document is to minimize risk to space programs in the area of electromagnetic compatibility (EMC).
Application
Document Applicability
This document is applicable to launch and space vehicles, their units and subsystems, plus the associated ground, airborne or spaceborne operational and support elements of the space system. This document does not apply to the facilities which house ground system segments of space systems (see MIL-STD-1542), nor does it apply to printed wiring board assemblies or individual microcircuits.
Requirement Applicability
The primary Requirements (e.g., 4.1, 6.05, 7.7), subrequirements (e.g., 4.2c2, 6.10c3, 7.1c1), verification methods (e.g., 4.3d1, 6.14d2, 7.7d) and tailoring (e.g., 4.1e1, 6.03e, 7.3e3) given in Sections 4 to 7 of this document are applicable in accordance with Table 1.2.2-1. They are also portion marked in the text in accordance with the explanation at the beginning of Table 1.2.2-1. All paragraphs under a primary Requirement have the same applicability as given at the primary Requirement title, unless otherwise marked.
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| contributor author | AIR FORCE - 02 - Air Force Network Integration Center (AFNIC) | |
| date accessioned | 2017-09-04T16:50:07Z | |
| date available | 2017-09-04T16:50:07Z | |
| date copyright | 06/13/2008 | |
| date issued | 2008 | |
| identifier other | WNDQJEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/113734 | |
| description abstract | Purpose The purpose of this document is to minimize risk to space programs in the area of electromagnetic compatibility (EMC). Application Document Applicability This document is applicable to launch and space vehicles, their units and subsystems, plus the associated ground, airborne or spaceborne operational and support elements of the space system. This document does not apply to the facilities which house ground system segments of space systems (see MIL-STD-1542), nor does it apply to printed wiring board assemblies or individual microcircuits. Requirement Applicability The primary Requirements (e.g., 4.1, 6.05, 7.7), subrequirements (e.g., 4.2c2, 6.10c3, 7.1c1), verification methods (e.g., 4.3d1, 6.14d2, 7.7d) and tailoring (e.g., 4.1e1, 6.03e, 7.3e3) given in Sections 4 to 7 of this document are applicable in accordance with Table 1.2.2-1. They are also portion marked in the text in accordance with the explanation at the beginning of Table 1.2.2-1. All paragraphs under a primary Requirement have the same applicability as given at the primary Requirement title, unless otherwise marked. | |
| language | English | |
| title | SMC-S-008 | num |
| title | ELECTROMAGNETIC COMPATABILITY REQUIREMENTS FOR SPACE EQUIPMENT AND SYSTEMS | en |
| type | standard | |
| page | 123 | |
| status | Active | |
| tree | AIR FORCE - 02 - Air Force Network Integration Center (AFNIC):;2008 | |
| contenttype | fulltext |