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Viewing 1 to 30 of 694
HISTORICAL
1968-10-01
Standard
AIR999
In this report, "Cryogenically Fueled Dynamic Power Systems" include all open cycle, chemically fueled, dynamic engine power systems which utilize cryogenic fuels and oxidizers. For nearly all practical present day systems, this category is limited to cryogenic hydrogen or hydrogen-oxygen fueled cycles with potential in future, more advanced systems for replacement of oxygen by fluorine. Excluded from the category are static cryogenic systems (e.g., fuel cells) and chemical dynamic power systems which utilize earth storable propellants.
CURRENT
2011-08-03
Standard
AIR999A
In this report, "Cryogenically Fueled Dynamic Power Systems" include all open cycle, chemically fueled, dynamic engine power systems which utilize cryogenic fuels and oxidizers. For nearly all practical present day systems, this category is limited to cryogenic hydrogen or hydrogen-oxygen fueled cycles with potential in future, more advanced systems for replacement of oxygen by fluorine. Excluded from the category are static cryogenic systems (e.g., fuel cells) and chemical dynamic power systems which utilize earth storable propellants.
2013-10-22
WIP Standard
AIR5654A
This handbook is intended to accompany or incorporate AS5643 IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications, AS5643/1 S400 Copper Media Interface Characteristics over Extended Distances, AS5657 Test Plan/Procedure for AS5643 IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications, AS5706 Test Plan/procedure for AS5643/1 S400 Copper Media Interface Characteristics Over Extended Distances, and ARD5708 Frequently Asked Questions about IEEE-1394b and SAE AS5643. In addition, full understanding of this handbook also requires knowledge of IEEE-1394-1995, IEEE-1394a and IEEE-1394b standards. This handbook contains detailed explanations and architecture analysis on AS5643, bus timing and scheduling considerations, system redundancy design considerations, suggestions on AS5643-based system configurations, cable selection guidance, and lessons learned on failure modes.
HISTORICAL
2003-06-06
Standard
AIR5532
This SAE Aerospace Information Report (AIR) defines a Generic Aircraft-Store Interface Framework (GASIF). This is a common framework for modeling and specifying aircraft-store logical interfaces. GASIF complies with the OSI Basic Reference Model (ITU-T Rec. X.200 | ISO/IEC 7498-1) in that it describes operations and mechanisms which are assignable to layers as specified in the OSI Basic Reference Model. This AIR provides a mapping of the Interface Standard for Aircraft-store Electrical Interconnection System (AEIS), MIL-STD-1760, in Appendix C.
CURRENT
2009-04-01
Standard
AIR5654
This handbook is intended to accompany or incorporate AS5643 IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications, AS5643/1 S400 Copper Media Interface Characteristics over Extended Distances, AS5657 Test Plan/Procedure for AS5643 IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications, AS5706 Test Plan/procedure for AS5643/1 S400 Copper Media Interface Characteristics Over Extended Distances, and ARD5708 Frequently Asked Questions about IEEE-1394b and SAE AS5643. In addition, full understanding of this handbook also requires knowledge of IEEE-1394-1995, IEEE-1394a and IEEE-1394b standards. This handbook contains detailed explanations and architecture analysis on AS5643, bus timing and scheduling considerations, system redundancy design considerations, suggestions on AS5643-based system configurations, cable selection guidance, and lessons learned on failure modes.
CURRENT
2012-05-03
Standard
AIR4903A
This section defines the scope of the document, provides a brief history of the Pi-Bus, discusses key features of the Pi-Bus, and provides an overview of the operation of the Pi-Bus. This document is a handbook intended to accompany AS4710 Pi-Bus standard. The purpose of this document is to provide information to aid users of the Pi-Bus, whether they be implementors of Pi-Bus controllers, architects of systems considering using the Pi-Bus, or programmers who must develop applications in a system which uses the Pi-Bus as the backplane communications bus. This document also provides rationale for many of the Pi-Bus requirements as defined in AS4710 and a discussion of potential enhancements that are being considered for the Pi-Bus.
HISTORICAL
1996-01-01
Standard
AIR4903
This section defines the scope of the document, provides a brief history of the Pi-Bus, discusses key features of the Pi-Bus, and provides an overview of the operation of the Pi-Bus. This document is a handbook intended to accompany AS4710 Pi-Bus standard. The purpose of this document is to provide information to aid users of the Pi-Bus, whether they be implementors of Pi-Bus controllers, architects of systems considering using the Pi-Bus, or programmers who must develop applications in a system which uses the Pi-Bus as the backplane communications bus. This document also provides rationale for many of the Pi-Bus requirements as defined in AS4710 and a discussion of potential enhancements that are being considered for the Pi-Bus.
HISTORICAL
1996-11-01
Standard
AIR4980
The original purpose of this document was to establish interface requirements for modular avionics backplanes to be prototyped up to 1995. The document was issued as ARD50011 in September 1992. It is being reissued as an SAE Aerospace Information Report (AIR) in order to: Preserve the requirements for more than 2 years Support design of retrofits and avionics systems to be fielded in the years 1995 to 2000 Provide a baseline for updating the requirements of future integrated systems These requirements were and are intended to promote standardization of modular avionic backplane interfaces. These requirements have been driven predominantly, but not exclusively, by aerospace type military platforms.
CURRENT
2012-05-03
Standard
AIR4980A
The original purpose of this document was to establish interface requirements for modular avionics backplanes to be prototyped up to 1995. The document was issued as ARD50011 in September 1992. It is being reissued as an SAE Aerospace Information Report (AIR) in order to: Preserve the requirements for more than 2 years Support design of retrofits and avionics systems to be fielded in the years 1995 to 2000 Provide a baseline for updating the requirements of future integrated systems These requirements were and are intended to promote standardization of modular avionic backplane interfaces. These requirements have been driven predominantly, but not exclusively, by aerospace type military platforms.
CURRENT
1999-01-01
Standard
AIR1500
The following bibliography on lossy filters for use on electrical and electronic systems was prepared by the Lossy Filter Subcommittee AE-4C.2 of the Society of Automotive Engineers. The bibliography is in chronological sequence and is oriented toward the use of lossy materials to attenuate radio frequency noise on transmission lines.
HISTORICAL
1978-02-01
Standard
AIR1394
CURRENT
1976-02-01
Standard
AIR1406
CURRENT
2002-05-17
Standard
ARIR666
This document describes a secure internet facility for sending all types of aviation software using the world wide web (www). Software suppliers may use this document as a starting point for the construction of a secure web server utility. It provides sufficient flexibility and is compatible with numerous software distribution models. The file management structure is consistent with other ARINC standards for loadable software, and references ARINC 665 and ARINC 667 in particular.
CURRENT
2001-01-15
Standard
ARIR660A
This standard expands ARINC 660 to include industry-defined architectures for the CNS/ATM operating environment. These architectures are intended to meet long-term requirements (e.g., ADS-B, CPDLC, etc.) and provide growth for the future. Airlines support the implementation of these architectures for the long-term. This standard represents broad airline consensus for developing avionics equipment providing CNS/ATM operating capabilities.
CURRENT
1993-12-27
Standard
ARIR659
Defines standards for the transfer of digital data between components within an IMA cabinet. Includes the protocol and timing characteristics for a synchronous backplane data bus capable of transferring data at 60 Mbps using a data path that is two bits wide. The electrical characteristics and behavior expected of the participating modules are defined.
CURRENT
2014-01-10
Standard
ARIR660B
This document identifies and describes the aircraft avionics capability necessary for operation in the evolving Communications Navigation Surveillance/Air Traffic Management (CNS/ATM) environment expected for the FAA NextGen program, Single European Sky ATM Research (SESAR) program and considerations of the Japan Collaborative Actions for Renovation of Air Traffic Systems (CARATS). These capabilities are intended to satisfy the industry's long-term CNS/ATM operational objectives.
CURRENT
1995-12-15
Standard
ARIR660
Defines a set of standard aircraft avionics architectures that support a cost-effective evolution to the fully operational CNS/ATM environment. These architectures are intended to meet near-term requirements (e.g., FANS-1, SCAT-1, etc.) and provide growth for supporting the full CNS/ATM function set. This standard represents broad airline consensus for developing avionics equipment providing CNS/ATM operating capabilities.
2005-02-11
WIP Standard
ARIC755-3_ERR1
CURRENT
1987-01-05
Standard
ARIR609
This standard describes electrical power system design and performance standards brought about by extensive use of digital avionics. This Report provides guidelines for designers of aircraft power system components and of power utilization components, both avionics and power converters such as motors and heaters.
CURRENT
1989-10-01
Standard
ARIR413A
This standard provides guidance to airframe manufacturers concerning the utilization of aircraft electrical power. This standard covers the description of basic power characteristics, and detailed guidance concerning transient protection, interference control, and equipment installation considerations.
CURRENT
1995-10-09
Standard
ARIR428
This standard provides the framework for developing a set of requirements for an avionics data bus network. This standard is intended to provide system-level considerations for the development of such a network, which may include a mix of standard data buses and private data buses.
CURRENT
2014-09-05
Standard
ARP6012A
This document, the JAUS Compliance and Interoperability Policy (ARP6012), recommends an approach to documenting the complete interface of an unmanned system or component in regard to the application of the standard set. While non-SAE AS-4 JAUS documents are referenced in this ARP they are not within the scope of this document and should be viewed as examples only.
HISTORICAL
2009-04-15
Standard
ARP6012
This document, the JAUS Compliance and Interoperability Policy (ARP6012), recommends an approach to documenting the complete interface of an unmanned system or component in regard to the application of the standard set. While non-SAE AS-4 JAUS documents are referenced in this ARP they are not within the scope of this document and should be viewed as examples only.
CURRENT
2017-11-30
Standard
ARP497B
This recommendation establishes objectives for high performance control motors to be used with aeronautical and associated equipment in protective enclosures or completely within the shell of the aircraft so that they are subjected only to the internal climatic conditions of heat, cold, shock, vibration, altitude, and humidity. Control motors larger than size #23 are not covered in this document.
CURRENT
2013-03-25
Standard
ARP4242A
This SAE Aerospace Recommended Practice (ARP) establishes overall system electromagnetic compatibility (EMC) control requirements. EMC includes the following: Electromagnetic Environmental Effects (E3) Electrostatic Discharge (ESD) Electromagnetic Interference (EMI) Electromagnetic Vulnerability (EMV) Electromagnetic Pulse (EMP) Hazards of Electromagnetic Radiation to Ordnance (HERO) Hazards of Electromagnetic Radiation to Personnel (HERP) Hazards of Electromagnetic Radiation to Fuels (HERF) High Intensity Radiated Fields (HIRF) Lightning Protection Static Electricity TEMPEST This document is intended to be used for the procurement of land, sea, air, or space systems by any procurement activity. Tailoring of specific requirements is necessary and Appendix A has been provided for guidance.
CURRENT
2017-11-30
Standard
ARP4729A
This SAE Aerospace Recommended Practice (ARP) provides technical design and application information related to the generation, distribution, control, and utilization of aircraft 270 V DC electrical power systems and support equipment. This document also provides references and definitions to permit comparisons of various electrical systems and components.
HISTORICAL
2007-02-21
Standard
AIR5683
MIL-STD-1553 establishes requirements for digital command/response time division multiplexing (TDM) techniques on military vehicles, especially aircraft. The existing MIL-STD-1553 network operates at a bit rate of 1 Mbps and is limited by the protocol to a maximum data payload capacity of approximately 700 kilobits per second. The limited capacity of MIL-STD-1553 buses coupled with emerging data rich applications for avionics platforms plus the expense involved with changing or adding wires to thousands of aircraft in the fleet has driven the need for expanding the data carrying capacity of the existing MIL-STD-1553 infrastructure.
Viewing 1 to 30 of 694

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