Show simple item record

TECHNICAL REQUIREMENTS FOR WIRING HARNESS, SPACE VEHICLE

contributor authorAIR FORCE - 02 - Air Force Network Integration Center (AFNIC)
date accessioned2017-09-04T16:41:27Z
date available2017-09-04T16:41:27Z
date copyright06/03/2009
date issued2009
identifier otherVPDQJEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/104729
description abstractPurpose
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.
languageEnglish
titleSMC-S-020num
titleTECHNICAL REQUIREMENTS FOR WIRING HARNESS, SPACE VEHICLEen
typestandard
page29
statusActive
treeAIR FORCE - 02 - Air Force Network Integration Center (AFNIC):;2009
contenttypefulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record