Filter Results By:
Products
Applications
Manufacturers
Avionics
all aviation electronics assurance.
See Also: Flight, Aviation, Flight Inspection, AFDX, NAV/COMM
- Pickering Interfaces Inc.
product
PXI Dual Bus 74-Chan 2A Fault Insertion Switch, N/O Through Relays
40-190B-302
The Dual Bus, 74 Channel PXI Fault Insertion switch is part of our family of 2 Amp fault insertion solutions, The range includes modules with 74, 64 or 32 channels and single or dual fault buses. This version has normally open through relays, so in the default state, there are no paths between inputs and outputs for any signal channel. It is primarily designed for the simulation of fault conditions in automotive & avionics applications involving the reliability testing of safety critical controllers.
-
product
Control and Switch Modules
Mini Mux
Eclypse International Mini Mux Control and Switch Modules, plus Software Developer Kit (SDK) provides high density test circuit switching as a complement to the Eclypse Circuit Analyzers. The Mini Mux Switching gives the user the ability to test continuity and isolation in complex assemblies with thousands of circuit paths (such as avionic back planes and chassis), while minimizing the test equipment complexity and footprint.
-
product
Becker Transponder Test Fixture
TA-3400
This transponder test fixture is specific to the requirements for testing Becker Avionics Transponders and provides interface connectors for both the panel mount and remote systems. The panel also provides switches to implement Gillham code altitude as well as separate interfaces for an external parallel or serial encoder. The panel will interface with the RMU 5000 or standard control head. This fixture also comes with voltage and current meters along with an internal dimming source. This panel comes in the standard 19 inch rack width and measures 12 inches in depth.
-
product
UNMANNED SOLUTIONS
Hermes 450
The Hermes 450 Unmanned Aerial System (UAS) is a highly reliable, mobile and deployable unit with 15 years of service and more than 100,000 hours of flight time. The fully composite, fully operational Hermes 450 may be launched and recovered from both prepared and semi-prepared runways. This medium-size, multi-payload UAS can operate two payloads simultaneously and provide persistent surveillance with endurance in excess of 18 hours and up to 30 hours with the optional external fuel tanks. The Hermes 450 offers high operational versatility for both military and non-military use, with manual or fully autonomous flight capabilities and common, cutting-edge, redundant avionics.
-
product
Time-Triggered Ethernet / ARINC 664 Part 7 (AFDX®) / IEEE 802.3 Ethernet Deterministic Communications
TE2
Module TE2 is one of NAI's latest generation of advanced function Configurable Open Systems Architecture™ (COSA®) compatible modules. The TE2 is a certifiable, single-port, tri-redundant, deterministic Ethernet communications interface module that supports TTTech’s certifiable TTEthernet® End System product consisting of three traffic classes: SAE AS6802 (Time-Triggered Ethernet), ARINC 664 Part 7 (Avionics Full-Duplex Switched Ethernet (AFDX®), and/or IEEE 802.3 best-effort protocol. By supporting all three traffic classes, NAI's TE2 is the ideal solution for current users of IEEE 802.3 Ethernet, who plan to upgrade to Deterministic Ethernet (ARINC 664 Part 7 (AFDX®) or Time-Triggered Ethernet SAE AS6802) protocols in the future at any time without changing hardware.
-
product
Avionics Test & Simulation Software
Ballard CoPilot® is an intuitive, graphical software program that allows you to easily monitor, record, replay, analyze, and simulate avionics bus data. With CoPilot you can interact directly with data on multiple buses using Ballard avionics interface hardware or work with previously recorded data. This advanced program features powerful tools for development, testing, troubleshooting and maintenance of avionics equipment and systems.
-
product
AIS Air Data Test System
F-16
The primary function of the Air Data Test System (ADTS) is to perform testing and fault isolation of pneumatic-type Units Under Test (UUTs). To test a UUT, the operator connects the associated Line Replaceable Unit (LRU) Integrated Test Adapter (ITA) to the rackmount Avionics Intermediate Shop (AIS) test station. The operator connects the ADTS to the IAIS via an RS-232 Interface and then finally, connects the UUT to the ADTS using the supplied cables and hoses.
-
product
Simulation Systems
GSIM
The GSIM avionics IO platform builds on The Goebel Companyʼs long historyin computer architecture and realtime simulation. Weather your IOrequirements are simply driving a cluster of displays, or driving a fullcomplement of avionics IO, GSIM has the solution for you. GSIM providesthe highest IO count in single chassis rack mount or desktop configurations.GSIM configurations are delivered with Linux Real-time systems.
-
product
Single Bus 75-Channel 2A PCI Fault Insertion Switch
50-190-001
This PCI fault insertion switch range is available with 75, 64 or 36 channels. It is primarily designed for the simulation of fault conditions in automotive & avionics applications involving the reliability testing of safety critical controllers. The Stimulus/Measurement to UUT path is suitable for supporting CAN and FlexRay bus systems.
-
product
USB2.0 Module With 2 CAN Bus Nodes ARINC825 Compliant For Testing & Simulation of Avionic ARINC825/CAN Bus Systems
APU825-2
USB2.0 module with 2 CAN bus nodes ARINC825 compliant for testing and simulation of Avionic ARINC825/CAN bus systems.
-
product
Next Gen ARINC 615-3/615A Portable Data Loader
Model No. 11615-50
Aero Instruments & Avionics, Inc.
The Aero Instruments & Avionics 11615-50 Portable Data Loader (PDL) provides proven ARINC 615-3/ARINC 603 load technologies with additional ARINC 615A over Ethernet capability. This new addition to our product line is ideal for aircraft fleets preparing to use, or that are currently using 615A loadable equipment. Avionic data loads can be performed from Floppy Disk, CD, DVD, USB, or the internal solid state Mass Storage Device (MSD). The MSD can be loaded in advance to eliminate the distribution of disks/memory devices to airplanes while significantly reducing the time to perform the data load tasks. External media is verified before any load is executed. This saves valuable ground time by alerting the operator of any bad media before attempting the load. Our 11615-50 PDL is easy to read and easy to use. All functions are performed using the high resolution 5” TFT LCD display and four large “Soft Buttons”. Together, they provide simple navigation to the selected loadable software and straightforward load status messages. Call Jim Krey for a quote: 716-694-7060 ext. 322
-
product
Microprocessors
CAES specializes in digital hardware design for commercial and aerospace applications. Our processing solutions are ideal for spacecraft on-board computers, payload processing, nuclear power plant controllers, critical transportation systems, high-altitude avionics, medical electronics and X-ray cargo scanning.
-
product
Ethernet & NLINE: Real-Time 1553 & ARINC Converter/Bridges
Alta’s Ethernet (ENET & NLINE) Avionics converters are the first and most unique Ethernet appliances in the industry. A real-time UDP server engine (no IP software stack like most other products on the market) provides direct data buffer and transmission control of MIL-STD-1553 and ARINC-429 interfaces.
-
product
Multiprotocol PCI/104-Express Interface Board
8000PCIe104
The EXC-8000PCIe104 is a multiprotocol PCI/104-Express interface board for embedded applications or avionics test and simulation applications. Each board holds up to four independent modules and 10 discrete channels.
-
product
PMC Module With 2 Or 4 CAN Bus Nodes ARINC825 Compliant For Testing & Simulation Of Avionic CAN Bus Systems
AMC825-x
ARINC825 (CAN bus) Test & Simulation module for PMC with 2 or 4 electrically isolated CAN bus nodes operating concurrently at CAN bus high speed bit rate of up to 1Mbit/s. The AMC825-x PCI Mezzanine Card (PMC) can work either with full functionality as an active CAN node for testing and simulating or in Listening Only mode for monitoring and recording purposes.
-
product
Avionics Supply Simulation System
Spitzenberger & Spies GmbH & Co. KG
Simulation of voltage variations. Simulation of frequency variations. Creation of practical disruptions
-
product
Avionics Communications Test
Astronics communications test sets for aircraft keep your radio, wireless, and navigation communications running at peak performance. Write test program sets once and deploy them instantaneously everywhere – whether your test set is in the factory, at the depot, or in facility operation.Deployed globally for nearly 20 years, Astronics communications testers deliver the dependability you require to ensure critical communications safety and security.
-
product
2 Channels, MIL-STD-1553, Dual Redundant, Transformer Coupled, Assisted Mode Capable (AMC)
FTB
MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed for use with military avionics, but has also become commonly used in spacecraft On-Board-Data-Handling (OBDH) subsystems, both military and civil. It features a dual, redundant, balanced-line, physical layer; a (differential) network interface; time division multiplexing; half-duplex command/response protocol; and up to 31 remote terminals (devices).
-
product
CPCI Avionics Bus Card
Avionics Bus Card is high end ARM core based MILBUS Communication Board. It is suitable for high speed Data Acquisition, Simulation, ATE applications. This board have MIL1553B, ARINC429, CCDL, digital I/O interface, USB, RS232, Ethernet interface and external bus interface. Board is well suitable for special type data acquisition & processing application. Board is based CPCI architecture and can be used with CPCI or PXI backplane. Rear IO Board is used to interface all IO’s of the board from Rear Side.
-
product
STANAG3910/EFEX Modules
AIM’s STANAG3910/EFEX test, simulation, monitoring and analysis modules use our field proven Common Core hardware design giving you the best performance, best feature set and highest functional integration on the market. The use of SoC (System on Chip) based core designs with multiple processors for real time bus protocol and application support, massive memory and IRIG-B time code encoder/decoder functions are standard. The latest versions also support avionics discrete I/O. Configurations with dual redundant concurrent HS/LS Bus Controller (BC), Multiple Remote Terminals, and Chronological/Mailbox Bus Monitor operation with full HS/LS protocol error injection/detection, multi-level triggering, advanced capture/filtering and real time bus recording, time stamping and physical bus replay ensure your bus integrity. Support for EFAbus Direct Digital Links (DDL), Fibre Optic DDL (FODDL) and EFAbus Express extensions (Mixed Mode and Dual Mode operation) are available. To support the French ‘Rafale’ aircraft, modules are available with an Electrical Front End. Single Function variants support cost effective solutions. Each module is delivered with a Board Support Package (BSP) containing the onboard driver software, a full Application Programming Interface (API) and detailed getting started and programming guides. Powerful PBA.pro databus test and analysis software is optionally available for all our STANAG3910 modules.
-
product
AC Power Sources
AMETEK Programmable Power, Inc.
AMETEK Programmable Power's AC power sources range from 800VA to 480kVA. From compliance test systems to rack-mounted industrial power subsystems, AMETEK Programmable Power is the leader in the design and manufacture of precision, programmable AC power sources used in R&D, test and measurement, avionics testing, inverter testing, arbitrary waveform generation, bulk power and power conditioning applications across a wide variety of industrial segments.
-
product
Compact PCI Express (3U) Generic Carrier Card
ACCx-1
To complement the wide range of interface modules for dedicated Avionics Databuses and Networks, AIM offers a range of Carrier modules for the use of AIM or any 3rd Party PMC and XMC module on various backplanes.
-
product
PXI Single Bus 64-Ch 2A Fault Insertion Switch
40-190B-101
The Single Bus, 64 Channel PXI Fault Insertion switch is part of our family of 2 Amp fault insertion solutions, The range includes modules with 74, 64 or 32 channels and single or dual fault buses. This version has normally closed through relays, so in the default state, there is a path between input and output for all signal channels. It is primarily designed for the simulation of fault conditions in automotive & avionics applications involving the reliability testing of safety critical controllers.
-
product
Inertial Systems
ACEINNA’s inertial systems provide end-users and systems integrators with fully-qualified MEMS-based solutions for measurement of static and dynamic motion in a wide variety of challenging environments, including; avionics, remotely operated vehicles, agricultural and construction vehicles, and automotive test.
-
product
PXI Single Bus 32-Ch 2A Fault Insertion Switch
40-190B-201
The Single Bus, 32 Channel PXI Fault Insertion switch is part of our family of 2 Amp fault insertion solutions, The range includes modules with 74, 64 or 32 channels and single or dual fault buses. This version has normally closed through relays, so in the default state, there is a path between input and output for all signal channels. It is primarily designed for the simulation of fault conditions in automotive & avionics applications involving the reliability testing of safety critical controllers.
-
product
HIRF Testing
High Intensity Radiated Fields (HIRF) testing simulates high RF peak pulsed and average fields typical of radar environments and is integral to the certification of flight essential avionics systems. L3 Cincinnati Electronics (L3 CE) can perform HIRF testing from 400 MHz to 18 GHz (with traditional average field testing from 10 kHz to 40 GHz).
-
product
Avionics Suite Tester
Based on order from the Navy, Data Patterns developed the complete Automated Test Equipment required for validating all the Line Replaceable Units (LRUs) utilized in the Seaking Helicopter. The upgrade was carried out at multiple Naval bases in India.
-
product
ARINC 429 Interface CPCI Card
RAR-429 Series
The RAR-429 module is a rugged, reliable, full featured, CompactPCI module designed to provide a stand-alone, ARINC 429 interface for avionics applications. Up to 16 ARINC429 channels are supported on a 3U CompactPCI module. The RAR-429 offers full functional test, simulation, and monitoring for ARINC 429 test and simulation applications.
-
product
Air Data Calibration Test System (ADCTS)
ADCTS-1000 Series
TestVonics Air Data Calibration Test System (ADCTS) is high precision advanced Secondary Air Data Controller-Monitor system. The ADCTS-1000 Series is a self-contained maneuverable rack mounted air data management system. The ADCTS is used in calibration labs, avionics engineering and avionics/instrument shops. The system is designed to perform both manual or automated test and calibration routines for a variety of air data test equipment (ie. test sets, air data computers, altimeters, airspeed indicators and line replaceable units). The ADCTS can be configured for use in both commercial and military environments.
-
product
Portable Avionics Interfaces for USB 2.0
These versatile interfaces are suitable for a wide range of applications in the lab and in the field. They support maximum data throughput on all channels and have a large 32 MB built-in memory. All power necessary for operation is provided via the single USB port. Plug and Play and Hot Swap features make them easy to install and move between computers.
-
product
1 Channel, MIL-STD-1553, Dual Redundant, Transformer Coupled, Assisted Mode Capable (AMC)
FTA
MIL-STD-1553 is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed for use with military avionics, but has also become commonly used in spacecraft On-Board-Data-Handling (OBDH) subsystems, both military and civil. It features a dual, redundant, balanced-line, physical layer; a (differential) network interface; time division multiplexing; half-duplex command/response protocol; and up to 31 remote terminals (devices).
