Search Results

Standard

Validation Methods For MIL-STD-1760D Mission Stores

2014-09-29

CURRENT

AS42701

This document establishes techniques for validating that a mission store complies with the interface requirements contained in MIL-STD-1760 Revision D.

Standard

Considerations for future more electric aircraft electric power systems

2011-05-06

WIP

AIR6198

This activity is focused on more electric and all electric type power systems for air vehicles. The scope of which includes source, distribution and user contributions to electrical power quality, failure modes, coordination, system reliabilty and robustness, impacts of being flight critical and the gaps which exist in present standards and guidance documents.

Standard

Recommendations and Background Material for Battery Package Testing

2020-11-04

WIP

AIR6840

AS 6413 and slash sheets /1 & /2 hold the main information for testing of battery packaging. This document holds further information and expansion of philosophy, clarification etc. surrounding the testing and industry needs.

Standard

Nitrogen Absorption/Desorption (Gas Dissolution) in Aircraft Shock Absorbers

2019-04-18

WIP

AIR6942

This document outlines the current state of the art in the understanding of gas in solution in shock absorber oils in unseperated shock absorbers. A literature review, overview of Henry's law, Henry's law coefficients for known gas and oil couples, in-service operational problems, lessons learned, and potential future work will be discussed in the document.

Standard

Landing Gear Based Weight and Balance Systems

2019-04-18

WIP

AIR6941

This document outlines historical systems which have used the landing gear as a sensor or installation point for full aircraft weight and balance systems. A number of systems have been developed, installed, certified, and placed in service but few systems remain in regular use. The document will capture the history of these systems, reasons (where known) for their withdrawal from service, and lessons learned.

Standard

Landing Gear Instrumentation for In-Service Loads Measurement

2016-11-03

WIP

AIR6805

This document will outline existing best practices in the instrumentation of landing gears for in-service operation (including flight test, operational loads monitoring, etc.).

Standard

Runway Condition Monitoring Systems

2022-04-13

WIP

AIR6697

This report will document Runway Condition Monitoring systems that provide information intended to reduce or eliminate aircraft runway excursions or overruns that may occur as a result of poor runway conditions.

Standard

Digital Avionics Fiber Optic Transmitters, Receivers and Transceivers for Aerospace Applications

2022-04-05

WIP

AIR7057

This information report is useful for personnel involved in the design, manufacturing, and/or use of digital fiber optic transmitters, receivers, and transceivers for aerospace applications

Standard

Fiber Optics and Applied Photonics Definitions

2020-01-30

WIP

AIR7366

A single depository for fiber optic and applied photonic definitions.

Standard

SAFE-LIFE LIMITS FOR LANDING GEAR STRUCTURES

2018-04-26

WIP

AIR6949

This document describes the approaches taken to define safe-life limits for the management of fatigue in landing gear structures, and the substantiation of those limits through full-scale fatigue testing. The safe-life scatter factors considered in a range of military and civil regulatory standards are also reviewed.

Standard

Aerospace Epoxy Technologies

2019-04-05

WIP

AIR7993

To detail the different epoxy types available for different aerospace applications which require different temperature ranges. Explain incoming/final inspection requirements and storage requirements. Examine the epoxy chemical make up with explanations of purpose in performance.

Standard

Advanced methods for Wire Selection and Sizing for Aerospace applications

2019-05-30

WIP

AIR7497

This SAE Aerospace Information Report is intended to provide advanced methods for wire selecting and sizing in aerospace application as a continuation of AIR6540, Fundamentals in Wire Selection and Sizing for Aerospace Applications. Also, it will provide valuable information for the electrical design engineer to verify the proper wire selection and validate a set of system design requirements which includes meeting environmental and installation constraints.

Standard

Aerospace Electrical Power System Stability

2018-09-10

WIP

AIR8445

EPS stability is an essential property that defines EPS ability to provide secure operation under required range of operation scenario. Power system stability is defined as “the ability of an electric power system, for a given initial operating condition, to regain a state of operating equilibrium after being subjected to a physical disturbance, with most system variables bounded so that practically the entire system remains intact”. This is applicable for AC and DC systems and has to address steady state conditions, transient conditions as well as high power loads connection / disconnection on the network.

Standard

FIBER OPTIC DESIGN GUIDELINES FOR AEROSPACE

2018-10-18

WIP

AIR8448

This document provides guidance on key areas of system design to achieve high performance and high reliability for mission critical aerospace systems and platforms. The fundamental element of a reliable, functional aerospace fiber optic application is the system design. It is the system designers’ task to define the methods, components, installation and processes supporting the transmission of the optical signal through the platform, while providing a physical layer with the necessary performance, reliability, and readiness for the application.

Standard

CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, SIZES 12, 16, 20, 22 AND 23 (FOR MICRO MINIATURE CONNECTORS)

2017-09-28

WIP

AS39029/127

CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, SIZES 12, 16, 20, 22 AND 23 (FOR MICRO MINIATURE CONNECTORS)

Standard

CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, SIZES 12, 16, 20, 22 AND 23 (FOR MICRO MINIATURE CONNECTOR)

2017-09-28

WIP

AS39029/128

CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, SIZES 12, 16, 20, 22 AND 23 (FOR MICRO MINIATURE CONNECTOR)

Standard

Contacts, Electrical Connector, Socket, Crimp Removable, Shielded, Size 16, (for MIL-C-24308 Connectors)

2021-10-12

WIP

AS39029/66

This project is being requested to convert MIL-C-39029/66 to an SAE standard so that this contact can be called out as a requirement in MIL-DTL-24308/41 and /42.

Standard

Contacts, Electrical Connector, Pin, Crimp Removable, Shielded, Size 16, (for MIL-C-24308 Connectors)

2021-10-15

WIP

AS39029/65

This project is being requested to convert MIL-C-39029/65 to an SAE standard so that this contact can be called out as a requirement in MIL-DTL-24308/41 and /42.

Standard

CONTACT, ELECTRICAL CONNECTOR, DIFFERENTIAL QUADRAX, SOCKET, SIZE 8, MIL-DTL-38999 SERIES I, III & IV

2011-05-11

WIP

AS39029/120

This request is to establish a new 39029 slash sheet to define a size 8 Quadrax socket contact.

Standard

WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE INSULATED, LOW FLUORIDE, SMOOTH SURFACE, NORMAL WEIGHT, SILVER-COATED COPPER, 200 °C, 600 VOLT, ROHS

2019-07-15

WIP

AS22759/70

New detailed sheet to AS22759 for extreme aerospace environments