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Guided Wave Radar Level Transmitter
2291
The 2291 Guided Wave Radar level transmitter is designed for continuous level measuring of conductive or non-conductive liquids, pulps and solids. The 2291 level gauge operates based on the well-known TDR (Time Domain Reflectometry) principle. Micropulses are sent along a probe guide at the speed of light. As soon as the impulse reaches the surface of the medium, it is reflected back to the electronic module. Level distance is directly proportional to the flight time of the impulse.
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Flight Inspection System
CARNAC
Compliant with ICAO, CARNAC Flight Inspection System enables flight inspection of all types of navaids: ILS, MKR, VOR, VHF, DME, Radars, VASI, PAPI, NDB, TACAN, MLS, GNSS procedures, etc. CARNAC is a compact cost saving solution designed to privilege efficiency and high precision avoiding heavy aircraft modifications and decreasing flight inspection time. It features advanced functions such as real-time processing, high-quality flight reports, calibration and remote control of the receivers, modularity, multi-missions and multi-navaids capabilities, automatic flying measurements procedures.
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One, Two, or Four Dual Redundant Interface MIL-STD-1553A/B Test & Simulation Module for PXI Express
PXIe-1553
Avionics Interface Technologies
1, 2, or 4 dual redundant MIL-STD-1553 bus interfaces Concurrent BC, multiple RT (31), and BM operations Full error injection and detection • Data capture filtering, 100% bus recording, and physical bus replay Multi-level Trigger for Capture/Filtering IRIG-B Time Encoder/Decoder Real-Time Recording and Physical Bus Replay Application interfaces supporting C, C++, C#, and .NET development Device Driver Support for: Windows, Linux, and LabVIEW Real Time (others provided on request) 10 high voltage (up to 30V) programmable DIO lines Flight Simulyzer GUI Analyzer software
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Innovative Multiple - Object Tracking Radar
iMOTR
We have advanced the multiple-object tracking radar concept with an innovative application to meet today’s test range needs. The iMOTR features enhanced clutter suppression capabilities to deliver clearer, more accurate assessments of object launch trajectory and flight path data on airborne and low flying objects. This tracking information can then be handed-off to other radars or data collection sensors in real-time. The system is also better equipped to provide precision time, space, and position information (TSPI) data of multiple objects in flight over a wider field of regard than the current test range radars in service.
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SEM- Based Dectors
ScintiFast™
ScintiFast™ is El-Mul’s flagship scintillator technology enabling the next generation of detectors with shorter response time and higher sensitivity. Recently released, ScintFast™ has the highest available photon yield for the nanosecond scintillator category. ScintiFast™ is the scintillator of choice for detectors in SEM-based tools for the semiconductor market as well as in Time of Flight Mass Spectrometry instruments.
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Data Recorder and Playback System
Curtiss-Wright Defense Solutions
The proliferation of sensors in today’s Intelligence, Surveillance and Reconnaissance (ISR) applications has increased the need for recording and playing back multiple channels of high-speed sensor data. Often times these ISR platforms are airborne which present certain environmental requirements that must be met for the system to be flight ready.
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Optical Sensor Test
For optical sensor test Cohu offers a variety of solutions being driven by requirements for tri-temp, parallelism and stimulus spacing. Customized optical stimulus units are integrated into Cohu’s test handling systems. For light detector test, we implement different types of light sources, such as infrared, ambient- and colored light. We offer different solutions for 3D image sensors combining emitter and receiver tests of LiDAR, Time of Flight and Structured Light devices.
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MIL-STD-1553 Test & Simulation Interface for PCI Express
PCIe-C1553
Avionics Interface Technologies
Dual redundant, single, dual or quad stream configurationsSoftware selectable Transformer, Direct, and Bus Stub Coupling Modes - Concurrent Bus Controller, 31 Remote Terminals, & Bus monitor operation - Full error injection and detection - Multi-level triggers for capture and filtering - Ten high voltage (up from 30V) programmable DIO lines - IRIG-B time code encoder/decoder with free-wheeling mode - Real-Time recording and physical bus replay - x1 Lane PCI Express Host Interface (x4 Physica...show more -
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Dynamic Data Simulator
LS-70-S
The Lumistar LS-70-S PCI Dynamic Data Simulator allows complex data streams to be generated for evaluation of bit synchronizers and PCM decommutator performance. It can also be used for uplink command generation to vehicles in flight, checkout of complete telemetry links, and playback of archived hard drive data in any format with the appropriate dll. The PCI board is only 7 inches long and contains the dynamic simulator and IRIG Time Code Generator.
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MIL-STD-1553 Interface Board
EXC-4000VME/MCH-x / EXC-4000VXI/MCH-x
The EXC-1553VME/MCH and EXC-1553VXI/MCH cards are based on a MIL-STD 1553 certified "Summit" chip used in many flight critical systems. Each dual redundant channel supports both MIL-STD-1553A and MIL-STD 1553B protocols. Up to eight channels may be programmed individually to operate as a Bus Controller, Remote Terminal, Bus Monitor, or Remote Terminal / Concurrent Bus Monitor. The 32 K x 16 of RAM allotted to each channel for the storage of data and control parameters may be updated in real time.
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Sound Velocity, Temperature and Pressure for Underwater Vehicles.
UV-SVP
Designed for Underwater Vehicles where space is at a premium, the UV-SVP is based on the Valeport miniSVS. Incorporating Valeport’s class-leading time of flight sound speed sensor, a PRT temperature sensor and a 0.01% pressure sensor in a compact package weighing just 750 grams (in air), the lightweight titanium housing gives a depth rating of 3000m. A wide range (9-30V DC) isolated power supply and RS232 communications complete the package.
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ARINC 429 PMC Interface Module
PMC-429
Avionics Interface Technologies
4, 8, 16, or 32 Software Programmable Tx/Rx ChannelsProgrammable High/Low Speed Operation - Concurrent operation of all Tx/Rx Channels at high data rates - Conduction-cooling and/or conformal coating available - Designed for extended temperature operations - Rate-oriented Label Transmission - Label Selective Trigger for Capture/Filtering - IRIG-B Time Code Encoder/Decoder for Data Correlation - ANSI Application Interface supporting C++, C#, and .net DevelopmentDevice Driver Support: Windows, Linux, VxWorks, and other operating system - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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ST VL6180X Time of Flight Sensor
SEN-36001
Highly integrated breakout board for the ST Micro VL6180X Time of Flight (ToF) range finder sensor. This sensor has many uses in the robotics, cell phone and gesture recognition space. It has two programmable GPIO pins, and most importantly, measures absolute distance up to 100mm. The SEN-36001 includes a VL6180X IC centered between two 4-40 sized mounting holes with onboard 2.8V LDO and voltage translation to handle interface voltages from 3V to 5V. The board is interfaced via an I2C interface...show more -
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MIL-STD-1553 PMC Interface Module
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...show more -
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ARINC 429 Test & Simulation Instrument for PXI
PXI-C429
Avionics Interface Technologies
4, 8, 16, or 32 Software Programmable Tx/Rx ChannelsProgrammable High/Low Speed Operation - Concurrent operation of all Tx/Rx Channels at high data rates - Full error injection and detection • Data capture filtering, 100% bus recording, and physical bus replay - Rate-oriented Label Transmission - Label Selective Trigger for Capture/Filtering - IRIG-B time code encoder/decoder with free-wheeling mode - Time Synchronization to PXI 10MHz reference clock - Application Interface supporting C/C++, C# and VB.NET Development - Device driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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ARINC 429 Test & Simulation Interface for PCI Express
PCIe-C429
Avionics Interface Technologies
4, 8, 16, or 32 Software Programmable Tx/Rx Channels - Programmable High/Low Speed Operation - Concurrent operation of all Tx/Rx Channels at high data rates - Full error injection and detection • Data capture filtering, 100% bus recording, and physical bus replay - Rate-oriented Label Transmission - Label Selective Trigger for Capture/Filtering - IRIG-B time code encoder/decoder with free-wheeling mode - Application Interface supporting C/C++, C# and VB.NET Development - Device driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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Flight Control System Test Platform
The Flight Control System Test Platform provides a hardware in-the-loop (HIL) closed-loop test environment for dynamic and maintenance testing of Flight Control Systems (FCS) of both commercial and military aircraft. The system simulates control surface activities from multiple combinations of rudder, flaps, elevator, aileron, and engine controls to the FCS. The system delivers repeatable, cost-effective testing in a fraction of the time needed with typical in-house simulation test systems.
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ARINC 664 Part 7 Test & Simulation Interface for PCI Express
PCIe-C664-V2
Avionics Interface Technologies
Supports IEEE 802.3 10/100/1000 Mbit/s Full-Duplex Ethernet links - Utilizes SFPs to support both copper and optical interfaces - Simulates multiple ARINC 664 End Systems - VL traffic shaping and input VL redundancy management - Supports up to 4K Output VLs and 4K Input VLs - Supports up to 16K Sampling & Queuing output message ports and up to 16K input Sampling & Queuing message ports - ARINC 653, UDP, IP protocols managed onboard - IRIG-B time code encoder/decoder - Automatic message s...show more -
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ARINC 664 Part 7 PXI Express Test & Simulation Instrument
PXIe-C664-V2
Avionics Interface Technologies
Supports IEEE 802.3 10/100/1000 Mbit/s Full-Duplex Ethernet links - Utilizes SFPs to support both copper and optical interfaces - Simulates multiple ARINC 664 End Systems - VL traffic shaping and input VL redundancy management - Supports up to 4K - Output VLs and 4K Input VLs - Supports up to 16K Sampling & Queuing output message ports and up to 16K input Sampling & Queuing message ports - ARINC 653, UDP, IP protocols managed onboard - IRIG-B time code encoder/decoder - Automatic message...show more -
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ARINC 664 Part 7 XMC Interface Module
XMC-664-V2
Avionics Interface Technologies
Supports IEEE 802.3 10/100/1000 Mbit/s Full-Duplex Ethernet links - Utilizes SFPs to support both copper and optical interfaces - Simulates multiple ARINC 664 End Systems - VL traffic shaping and input VL redundancy management - Supports up to 4K Output VLs and 4K Input VLs - Supports up to 16K Sampling & Queuing output message ports and up to 16K input Sampling & Queuing message ports - ARINC 653, UDP, IP protocols managed onboard - IRIG-B time code encoder/decoder - Automatic message s...show more -
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Vision app-based Sensor
NXT vegas
Imaging Development Systems GmbH
The app-based system makes it as versatile as a smartphone. With the integrated 1.3 MP CMOS sensor, an integrated liquid lens, LED illumination and a ToF sensor (Time of Flight) for distance measurement, it is fully equipped for many different image processing tasks. As a complete embedded vision component, it simplifies integrated design into custom device hardware and software. The board-level option is also very interesting for OEM equipment manufacturers.
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Sound Velocity Sensor
miniSVS
The Valeport miniSVS uses digital "time of flight" technology to provide the lowest noise, highest accuracy, best resolution sound velocity data available.
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Electronic Tachometers
1 1/4″, 2 1/4″ & 3 1/8″ Aircore Propeller tach for Rotax912/914 engines, connects to tach coil, calibrated to Propeller RPM, not Engine RPM! Custom color marking available, internal light optional! Hourmeter can be set to count engine time or flight time and preset to any numbers —(must be done at UMA facility)!—Standard setting 800rpm & above. White or Antique yellow dial with black numbers available, per request!
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MIL-STD-1553 USB & LAN Test & Simulation Module
UXI-1553
Avionics Interface Technologies
Dual redundant, single, dual, or quad stream configurationsConcurrent BC, 31 RTs, and BM operations - Physical Bus ReplayFull error injection/detection capabilities - Programmable trigger and capture - Programmable Bus Coupling and Output Voltage Levels - Onboard IRIG-B time code encoder/decoder for Synchronization - Time Synchronization to IEEE 1588 via Ethernet LAN port - 10 Discrete I/O Interfaces (5 Outputs / 5 Inputs) - Operates from a single USB or Ethernet LAN connection - Supports SAE AS4112/4114 protocol testing requirements- Flight Simulyzer™ GUI Analyzer software
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MIL-STD-1553 XMC Interface Module
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: Wind...show more -
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Time Domain Reflectometers
HL1100 Series
HYPERLABS HL1100 Series TDR instruments provide high-performance test and measurement capabilities for use in the field or in the lab. These instruments are used for applications such as fault detection in cables and interconnects, impedance characterization, time of flight analysis, water level measurement, and more.
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MIL-STD-1553 Test & Simulation Interface for PCI
PCI-C1553
Avionics Interface Technologies
Dual redundant, single, dual or quad stream configurationsSoftware selectable Transformer, Direct, and Bus Stub Coupling Modes - Concurrent Bus Controller, 31 Remote Terminals, & Bus monitor operation - Full error injection and detection - Multi-level triggers for capture and filtering - Ten high voltage (up from 30V) programmable DIO lines - IRIG-B time code encoder/decoder with free-wheeling mode - Real-Time recording and physical bus replay - PCI & PCIx Compatible, 3.3V and 5V Operati...show more -
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Data Monitoring System
1S663-001
The 1S663-001 Data Monitoring System was specifically developed for the Cessna Citation X and serves as the primary diagnostic tool for the aircraft?? electronic Logic Modules. The system is FAA certified for airborne operation. Aft compartment and cabin modules can be tested two at a time while remaining in place. The system is also capable of monitoring the fuel quantity system during flight.
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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.
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LIDAR & Direct Time of Flight
LIDAR (Light Detection and Ranging) is a sensor technology for remote object detection and ranging, using a light source and receiver. Emitted light pulses hit objects, reflect, and return to the LiDAR sensor system where the receiver detects the returning light pulse.
