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SMC-S-020
TECHNICAL REQUIREMENTS FOR WIRING HARNESS, SPACE VEHICLE
Year: 2009
Abstract: Purpose
These requirements set forth the general design and testing requirements for electrical wiring harnesses (see 6.1) and cable assemblies (see 6.2.4) that are to be installed in space vehicles.
Application
The wiring requirements covered by this document are applicable to wiring harnesses and accessories for the use in the interconnection of electrical and electronic equipment in space vehicles. These requirements may also be used to specify requirements for interconnect wiring on launch vehicles, intercontinental ballistic missiles, or other vehicles (see 6.1). For those applications the term "space vehicle" is to be interpreted as the applicable vehicle. This document may be tailored by the acquisition activity for the specific application or program prior to contract award.
Compliance with System Requirements
These requirements shall not relieve the contractor and subcontractors of the responsibility for complying with all the equipment, system performance, and reliability requirements as set forth in the applicable specifications and contract.
These requirements set forth the general design and testing requirements for electrical wiring harnesses (see 6.1) and cable assemblies (see 6.2.4) that are to be installed in space vehicles.
Application
The wiring requirements covered by this document are applicable to wiring harnesses and accessories for the use in the interconnection of electrical and electronic equipment in space vehicles. These requirements may also be used to specify requirements for interconnect wiring on launch vehicles, intercontinental ballistic missiles, or other vehicles (see 6.1). For those applications the term "space vehicle" is to be interpreted as the applicable vehicle. This document may be tailored by the acquisition activity for the specific application or program prior to contract award.
Compliance with System Requirements
These requirements shall not relieve the contractor and subcontractors of the responsibility for complying with all the equipment, system performance, and reliability requirements as set forth in the applicable specifications and contract.
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| contributor author | AIR FORCE - 02 - Air Force Network Integration Center (AFNIC) | |
| date accessioned | 2017-09-04T16:41:27Z | |
| date available | 2017-09-04T16:41:27Z | |
| date copyright | 06/03/2009 | |
| date issued | 2009 | |
| identifier other | VPDQJEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/104729 | |
| description abstract | Purpose These requirements set forth the general design and testing requirements for electrical wiring harnesses (see 6.1) and cable assemblies (see 6.2.4) that are to be installed in space vehicles. Application The wiring requirements covered by this document are applicable to wiring harnesses and accessories for the use in the interconnection of electrical and electronic equipment in space vehicles. These requirements may also be used to specify requirements for interconnect wiring on launch vehicles, intercontinental ballistic missiles, or other vehicles (see 6.1). For those applications the term "space vehicle" is to be interpreted as the applicable vehicle. This document may be tailored by the acquisition activity for the specific application or program prior to contract award. Compliance with System Requirements These requirements shall not relieve the contractor and subcontractors of the responsibility for complying with all the equipment, system performance, and reliability requirements as set forth in the applicable specifications and contract. | |
| language | English | |
| title | SMC-S-020 | num |
| title | TECHNICAL REQUIREMENTS FOR WIRING HARNESS, SPACE VEHICLE | en |
| type | standard | |
| page | 29 | |
| status | Active | |
| tree | AIR FORCE - 02 - Air Force Network Integration Center (AFNIC):;2009 | |
| contenttype | fulltext |