Refine Your Search

Topic

Search Results

Standard

MARK I AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM PART 2 ELECTRICAL INTERFACES AND FUNCTIONAL EQUIPMENT DESCRIPTION

2014-07-28
CURRENT
ARIC791P2-1
This document provides the interface definition of the Satcom system. Any signal crossing into or out of the communication system is documented to ease aircraft integration. ...Signals within the ARINC 791 Satcom system, and in particular, between the Modman and the Antenna Subsystem, are described to permit interchangeability between any Modman and any Antenna Subsystem.
Article

Viasat military-grade airborne SATCOM antenna achieves FAA certification, completes Air Force C-17 MACC testing

2018-07-31
The Viasat Global Mobile Antenna 5560-101 military-grade, Ku-/Ka-band, multi-network, multi-mode satellite communications antenna has demonstrated it can provide in-flight broadband connectivity to enable advanced situational awareness, en-route mission planning, and other applications that demand high forward and return link capacity. FAA DO-160G certification enables the antenna to be installed on select manned and unmanned military aircraft, while passing AFMC C-17 MACC tests demonstrates the antenna's ability to become certified for Air Force and FMS C-17 aircraft.
Standard

LOW-EARTH ORBITING AVIATION SATELLITE COMMUNICATION SYSTEMS

2018-10-01
CURRENT
ARIC771-1
This document sets forth the desired characteristics of the Iridium Low-Earth Orbiting (LEO) Aviation Satellite Communication (Satcom) System avionics intended for installation in all types of aircraft including commercial transport, business, and general aviation aircraft.
Standard

MARK 3 AVIATION SATELLITE COMMUNICATION SYSTEMS

2017-08-09
CURRENT
ARIC781-7
This document sets forth the desired characteristics of an aviation satellite communication (Satcom) system intended for installation in all types of commercial transport and business aircraft.
Standard

LOW-EARTH ORBITING AVIATION SATELLITE COMMUNICATION SYSTEM

2016-08-05
CURRENT
ARIC771
This document sets forth the desired characteristics of the Iridium Low-Earth Orbiting (LEO) Aviation Satellite Communication (Satcom) System avionics intended for installation in all types of aircraft including commercial transport, business, and general aviation aircraft.
Standard

COMMUNICATIONS AND NAVIGATION EQUIPMENT

1988-07-01
CURRENT
ARP4102/6
The equipment includes: a Communications: Ultra High Frequency (UHF), Very High Frequency (VHF), and High Frequency (HF) Radios, Cabin/Service Interphones, Public Address (PA), Select Call (SELCAL), Call Select (CALSEL), Satellite Communications (SATCOM). b Navigation: Very High Frequency Omnidirectional Range (VOR), Tactical Air Navigation (TACAN), Automatic Direction Finder (ADF), Distance Measuring Equipment (DME), Instrument Landing System (ILS), Markers (MKR), Omega, Very Low Frequency (VLF), Inertial Navigation Systems (INS), Inertial Reference Systems (IRS), Satellite Navigation (SATNAV), Low Range Radio Altimeter (LRRA). c Weather Radar d Data Link: Company, Air Traffic Control (ATC) Transponders (Mode-S) and others.
Technical Paper

Implementing Data Link Across the Pacific

1991-09-01
912235
It was agreed that the focus of effort would be directed to long-range operations over the Pacific Ocean utilizing the SATCOM system developed by Collins Radio, installed and certified by the Boeing Company on a 747-400 aircraft, and an INMARSAT satellite with digital data communications service provided by the COMSAT Corporation.
Technical Paper

FENSAP-ICE in Aid of Certification: From CFD to Flight Testing

2011-06-13
2011-38-0033
This work presents an example of the application of FENSAP-ICE to predict 45 minutes of ice accretion on a RC-26B aircraft fuselage retrofitted by the addition of a FLIR sensor and a SATCOM antenna. The predicted aerodynamic penalties are compared with recorded flight test data obtained with simulated ice shapes.
Technical Paper

Minimum Crew Certification Human Factors Issues and Approaches

1996-10-01
965510
This can include such additions as Flight Management System (FMS) and Global Positioning System (GPS) interfacing to Autopilots and Flight Directors, Multi-Function Control and Display Units (MCDU), Satellite Communications (SatCom) and High Frequency (HF) Data Links, Heads-Up-Display (HUD) technologies, and even complete three-to-two pilot flight deck conversions.
Standard

Communications and Navigation Equipment

2016-01-18
WIP
ARP4102/6A
Communications: Ultra High Frequency (UHF), Very High Frequency (VHF), and High Frequency (HF) Radios, Cabin/Service Interphones, Public Address (PA), Select Call (SELCAL), Call Select (CALSEL), Satellite Communications (SATCOM), b. Navigation: Very High Frequency Omnidirectional Range (VOR), Tactical Air Navigation (TACAN), Automatic Direction Finder (ADF), Distance Measuring Equipment (DME), Instrument Landing System (ILS), Markers (MKR), Omega, Very Low Frequency (VLF), Inertial Navigation Systems (INS), Inertial Reference Systems (IRS), Satellite Navigation (SATNAV), Low Range Radio Altimeter (LRRA).
Magazine

Aerospace & Defense Technology: September 2018

2018-09-01
Enhanced SATCOMs for Unmanned Aerial Systems The Bus Too Tough to Die Combating Infrared Threats on the Battlefield Optical Interconnect Design Challenges in Space High-Performance Computing for the Next-Generation Combat Vehicle Merging Antenna and Electronics Boosts Energy and Spectrum Efficiency Integrated Magneto-Optical Devices for On-Chip Photonic Systems Development of magneto-optical (MO) materials could lead to a range of nonreciprocal optical devices for emerging standardized photonic integrated circuit (PIC) fabrication processes.
Standard

AIR/GROUND CHARACTER-ORIENTED PROTOCOL SPECIFICATION

2016-08-10
CURRENT
ARIS618-8
This standard defines the Aircraft Communications Addressing and Reporting System (ACARS), a VHF data link that transfers character-oriented data between aircraft systems and ground systems. This communications facility enables the aircraft to operate as part of the airline's command, control and management system.
Technical Paper

Flight Tests Telemetry Link for Small and Medium Aircrafts

2005-11-22
2005-01-4137
It is common at the great aerospace companies or research centers to perform flight tests in facilities deployed for aircrafts and systems evaluation. These resources require high planning and investments comprising telemetry system, airborne and terrestrial equipments, calibration labs and specialized staff. It proposes in flight data acquisition means for support tests programs of aircrafts and airborne systems of low complexity in new developments. Also, it can be used as an optimization tool by introducing the telemetry efficiency concept applied to the development of new aircrafts where there are at least two prototypes read to fly.
Standard

AVIATION SATELLITE COMMUNICATION SYSTEM PART 2 SYSTEM DESIGN AND EQUIPMENT FUNCTIONAL DESCRIPTION

2012-06-27
CURRENT
ARIC741P2-11
This document describes the desired operational capability of the equipment as configured with the first generation Satellite Data Unit (SDU) to provide data and voice communications, as well as additional standards necessary to ensure interchangeability. Supplement 11 adds commentary on the commonality of physical interfaces between ARINC 741 systems defined for SwiftBroadband safety services and ARINC 741 systems defined only for the Inmarsat Classic Aero safety services. It adds the SwiftBroadband safety services to the SDU functional definition.
X