SAE Aerospace Standards

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Standard [CURRENT] 2023-03-27

SAE AS 5692/3:2023-03-27

ARC FAULT CIRCUIT BREAKER - AIRCRAFT, TRIP FREE, 1 TO 20 AMP, TYPE I

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Standard [CURRENT] 2023-03-27

SAE AS 5692/4:2023-03-27

ARC FAULT CIRCUIT BREAKER - AIRCRAFT, TRIP FREE, 25 TO 35 AMP, TYPE 1

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Standard [CURRENT] 2023-03-27

SAE AS 5692A:2023-03-27

ARC Fault Circuit Breaker ( AFCB), Aircraft, Trip-Free Single Phase and Three Phase 115 VAC, 400 Hz - Constant Frequency

The primary function of this specification is to cover the general requirements for manual reset trip-free arc fault/thermal circuit breakers for use in aircraft electrical systems conforming to ...

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Standard [CURRENT] 2018-09-13

SAE AS 5698A:2018-09-13

Space Power Standard

This standard defines the requirements and characteristics of electrical power for spacecraft. This standard also defines analysis, verification, and testing methodologies to be used to ensure ...

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Standard [CURRENT] 2021-04-14

SAE AS 5706A:2021-04-14

Test Plan/Procedure for AS5643/1 S400 Copper Media Interface Characteristics Over Extended Distances

This document establishes test plans/procedures for the AS5643/1 Slash Sheet. The AS5643/1 Slash Sheet establishes guidelines for the use of IEEE Std 1394-2008 as a data bus network in military ...

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Standard [CURRENT] 2010-08-26

SAE AS 5710A:2010-08-26

JAUS Core Service Set

This document defines a set of standard application layer interfaces called JAUS Core Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned ...

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Standard [CURRENT] 2022-09-08

SAE AS 5714A:2022-09-08

Minimum Performance Standard for Parts 23, 27, and 29 Aircraft Wheels, Brakes, and Wheel and Brake Assemblies

This SAE Aerospace Standard (AS) prescribes the Minimum Performance Standards (MPS) for wheel, brake, and wheel and brake assemblies to be used on aircraft certificated under 14 CFR Parts 23, 27 ...

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Standard [CURRENT] 2012-12-03

SAE AS 5716A:2012-12-03

Standard Electrical and Logical Interface for Airborne Fuzing Systems

This interface standard applies to fuzes/fuzing systems (referred to as fuzing system hereafter) in airborne weapons that use a MIL-STD-1760 type interface. It defines the powers, the discrete ...

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Standard [CURRENT] 2023-11-10

SAE AS 5722:2023-11-10

Cockpit Crew Oxygen Equipment for Use from 35000 to 45000 feet Altitude

This document covers minimum performance standards for protective equipment used on the flight deck during rapid decompression (5 to 30 seconds) up to a maximum pressure altitude of 45000 feet.

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Standard [CURRENT] 2023-05-22

SAE AS 5725C:2023-05-22

Interface Standard, Miniature Mission Store Interface

This SAE Aerospace Standard (AS) defines implementation requirements for the electrical interface between: a Aircraft carried miniature store carriage systems and miniature stores b Aircraft ...

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