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AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City: Recent submissions
Now showing items 121-140 of 323
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MIL-N-25161C (4)
Abstract: This specification covers an aerial pressure refueling nozzle, for use with "probe and drogue" type aerial refueling systems.Intended Use: The aerial pressure refueling nozzles covered by this specification ... -
MIL-STD-464C
Abstract: Purpose.
This standard establishes electromagnetic environmental effects (E3) interface requirements and verification criteria for airborne, sea, space, and ground systems, including associated ordnance. ...Subject(s) : E3 , Electrical bonding , Electromagnetic compatibility , Electromagnetic emission , Electromagnetic environment , Electromagnetic interference , Electromagnetic radiation hazards , Electromagnetic susceptibility , EMC , EMCON , EMI , EMP , ESD , Grounding , HERF , HERO , HERP , HPM , IMI , Inter-system electromagnetic compatibility , Intra-system electromagnetic compatibility , Lightning , Multipaction , P-static , RADHAZ , System , TEMPEST , -
MIL-HDBK-515 VALID NOTICE 2
Abstract: This document provides guidance on how to integrate the existing integrity processes within systems engineering, resulting in a more efficient and cohesive approach to engineering. In order to accomplish this, the Weapon ... -
DI-SESS-81768
Abstract: Use/relationship: The purpose of the Airworthiness Certification Criteria Report is to provide airworthiness certification criteria verification results. The data will be used to support program managers' ... -
MIL-R-83722/7
Abstract: The complete requirements for procuring the relay described herein shall consist of this document and the issue in effect of Specification MIL-R-83722 (USAF). -
MIL-B-5716B
Abstract: This specification covers one type of 35-millimeter radarscope image recording camera body designated type C-1A. The camera body is a component of the type O-15A camera system. Intended Use: This camera ... -
MIL-STD-1530C
Abstract: This standard describes the USAF Aircraft Structural Integrity Program (ASIP) which defines the requirements necessary to achieve structural integrity in USAF aircraft while managing cost and schedule risks through a series ...Subject(s) : aeroacoustics , aircraft structure , corrosion , cracking , damage tolerance , durability , economic life , fatigue , flight test , flutter , force management , ground test , loads , mass , nondestructive inspection (NDI) , probability of failure , proof test , risk , service life , static test , strength , sustainment , vibration , weight and balance , widespread fatigue damage , -
MIL-HDBK-500B VALID NOTICE 1
Abstract: This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.
Objective.
The objective of this handbook is to identify and ... -
MIL-C-83450A
Abstract: This specification covers the requirements for non-melting cloth used in the manufacture of special flying clothing. Intended Use: The cloth covered by this specification is intended for use in the fabrication ... -
MIL-C-87261
Abstract: This specification covers the requirements for chemical protective and flame, resistant fabric with activated carbon spheres laminated between polybenzimidazole/aramid blended woven outer layer cloth and knit inner layer ...Subject(s) : Activated carbon sphere , Aramid substrate , Carbon tetrachloride , Chemical agent protection , Cloth , Detergen exposure , Flame resistant , Laminated fabric , Launderings , Material , Nitrogen gas , Polybenzimidazole , Shrink , -
MIL-R-25988/3
Abstract: The complete requirements for procuring the o-ring described herein shall consist of this document and the issue in effect of Specification MIL-R-25988(USAF)
Purpose. The purpose of this specification sheet is ...