Showing results: 391 - 405 of 1700 items found.
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AD-LPCI-3488A -
LXinstruments GmbH
The IEEE488 standard, also known as GPIB, is a bus interface that connects devices to a computer to form an ATE system. GPIB was originally developed by Hewlett Packard and was recognized as an IEEE standard in 1978. The IEEE488.1-1978 standard defines the convention for electrical and mechanical bus properties, as well as the state diagram for each bus function. In 1987, another standard was derived from the original IEEE488.1-1978, which became known as IEEE488.2-1987.
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M3406A -
Keysight Technologies
Interface to the LRU in avionics test solution Up to four channel MIL-STD-1553 bus interface with full error injection and detection Concurrent Bus Controller, multiple Remote Terminals (31), and Bus Monitor operation capabilities Data capture filtering, 100% bus recording, and physical bus replay Variable output voltage signal and software selectable bus coupling modes 10 high voltage (up to 30 V) programmable DIO lines PXI trigger generation on 1553 bus events
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cPCIRepeat32 -
Dynamic Engineering
cPCIRepeat32 ( cPCI to PMC ) adapter / carrier converter card provides the ability to install up one PMC card into a cPCI slot designed for bus expansion. The J2 connector can be left off for non bus expansion positions.
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ABex TM-4070 DMM -
Konrad Technologies GmbH
The ABex TM-4070 is an ABex terminal module to interface with NI PXI-407x or PXIe-408x and gives the possibility to rout the DMM signals to the front connector and the Analog bus. The routing to the analog bus is software controlled and the signals are switched with reed relays.
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IIB-1553-CPCI -
Western Avionics Ltd.
The IIB-1553-CPCI is an intelligent interface card providing full MIL-STD-1553 test, simulation and bus analysis capability for the CompactPCI bus, with 1553A, 1553B, McAir and STANAG 3838 capability on a single card.The IIB-1553-CPCI supports concurrent Bus Controller (BC) and up to 31 Remote Terminals (RT) with Bus Monitor (BM). An additional stand-alone Chronological Bus Monitor (CBM) facility is also provided, with comprehensive multi-level triggering capability. Full error injection capability is provided in BC and RT modes,with full error detection in BC, RT, BM and CBM modes. The unit provides a dual redundant 1553 interface.2 Mbytes of dual ported RAM are supplied as standard. The board is supplied with C drivers in source code and Windows menu driven software.
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IIB-1553-PC104+ -
Western Avionics Ltd.
The IIB-1553-PC104+ is an intelligent interface card giving full MIL-STD-1553 test, simulation and bus analysis capability on the PC104+ bus, providing 1553A, 1553B, McAir and STANAG 3838 variants in a single card. The IIB-1553-PC104+ supports concurrent Bus Controller (BC) and up to 31 Remote Terminals (RT) with Bus Monitor (BM). An additional stand-alone Chronological Bus Monitor (CBM) facility is also provided, with comprehensive multi-level triggering capability. Full error injection capability is provided in BC and RT modes, with full error detection in BC, RT, BM and CBM modes. The unit provides a variable amplitude dual redundant 1553 interface. 2 Mbytes of dual ported RAM are provided. The board is supplied with C drivers in source code and Windows menu driven software as standard.
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PMC-1553 -
Avionics Interface Technologies
Dual redundant, single, dual, or quad stream configurationsTransformer & Direct Bus Coupling - Concurrent Bus Controller, 31 Remote Terminals, & Bus Monitor operation - Full error injection and detection - Multi-level trigger for capture and filtering - IRIG-B time code encoder/decoder - Ten high voltage (up to 30V) programmable DIO lines - Real-Time recording and physical bus replay - ANSI Application interface supporting C, C++, C#, and .NET development - Device driver support: Windows, Linux, VxWorks, & LabVIEW Real-Time (others on request) - Conduction-cooling and/or conformal coating available - Designed for extended temperature operations - 3.3v PMC (with 5V Tolerant I/O), 64-bit 33/66MHz - Rear (P14) and Front Panel Input/Output - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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XMC-1553 -
Avionics Interface Technologies
Dual redundant, single, dual, or quad stream configurations - Transformer & Direct Bus Coupling - Concurrent Bus Controller, 31 Remote Terminals, & Bus Monitor operation - Full error injection and detection - Multi-level trigger for capture and filtering - IRIG-B time code encoder/decoder - Ten high voltage (up to 30V) programmable DIO lines - Real-Time recording and physical bus replay - ANSI Application interface supporting C, C++, C#, and .NET development - Device driver support: Windows, Linux, VxWorks, & LabVIEW Real-Time (others on request) - Conduction-cooling and/or conformal coating availableDesigned for extended temperature operations - x1 Lane PCI Express Host Interface - Rear (P14) and Front Panel Input/Output - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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Euresys Inc.
Four CoaXPress CXP-12 connections: 5,000 MB/s camera bandwidthPCIe 3.0 (Gen 3) x8 bus: 6,700 MB/s bus bandwidthFeature-rich set of 20 digital I/O linesExtensive camera control functionsMemento Event Logging Tool
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Euresys Inc.
Four CoaXPress CXP-6 connections: 2,500 MB/s camera bandwidthPCIe 3.0 (Gen 3) x4 bus: 3,300 MB/s bus bandwidthFeature-rich set of 20 digital I/O linesFan-cooled heatsinkExtensive camera control functionsMemento Event Logging Tool
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E160-6U-2 -
VECTOR Electronics and Technology, Inc.
6U x 160mm Eurocard size for 96-pin DIN connectors.Voltage and ground bus around board perimeter on both sides. Bus surfaces solder coated for user convenience. For solder, Wire-Wrap or mixed wiring methods.Row and column legends provided.
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4616-1, 160-PIN VME64x -
VECTOR Electronics and Technology, Inc.
6U x 160mm Eurocard size for 160-pin DIN connectors. Pad per hole pattern both sides. Voltage and Ground bus both sides. Pad and bus surfaces solder-coated for user convenience. Row and column legends provided.