Flight
See Also: Flight Inspection, Avionics
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Gyro Pressure
Used to monitor the vacuum developed in the system that actuates the air driven gyroscopic flight instruments.
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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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Aerospace Systems And Technologies
The world's leading aircraft manufacturers and engine makers rely on Parker Aerospace's flight control, hydraulic, fuel-inerting, fluid-conveyance, thermal-management, pneumatic, and lubrication systems and components. Parker's systems and technologies expertise helps move customers' programs forward while increasing productivity and profitability.
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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 sequencing & periodic data generated onboard - Error Injection including Runt Frames, Short IFG, and Invalid MAC FCSDevice driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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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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Laser Distance Sensors (Time-of-Flight)
optoNCDT
Laser distance sensors are designed for non-contact distance measurements: laser gauges for measuring ranges up to 10m, laser distance sensors for up to 3,000m. These sensors are used for positioning and type classification in machine building and handling equipment.
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Compact PCI Multi-function Decommutator
LS-50-cP
The Lumistar LS-50-cP 3U Compact PCI Multi-function PCM Decommutator offers the greatest flexibility in the industry by incorporating up to 10 functions typically encountered in flight test applications in a single 3U Compact-PCI card slot. Five functions are achieved on the main board (PCM Simulator which can also operate as a BERT, PCM Decommutator, IRIG Time CodeReader, IRIG Time Code Generator, and the same 5 functions can be achieved on the LS-55-DB Multi-Function Decom Daughterboard. CVSD Voice Decoding and h.261 Video Decoding are achieved through software.
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ARINC 664 Part 7 Test & Simulation Interface for PCI
PCI-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 interfacesSimulates 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 sequencing & periodic data generated onboardError Injection including Runt Frames, Short IFG, and Invalid MAC FCS - 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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APU Test Set
H296G Series
The H296G Series is a flight line diagnostic tool that monitors selected parameters and provides engine control during APU trimming.
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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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MIL-STD-1553
The Avionic Interface MIL-STD-1553 products offer solutions for flight test instrumentation (FTI), for data acquisition, for protocol analysis, embedded IP solutions and COTS applications.
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Matrix-Assisted Laser Desorption/Ionization Time-of-Flight Mass Spectrometer
MALDI-8020
The MALDI-8020 is the latest in a long line of MALDI-TOF products from Shimadzu. This benchtop, linear MALDI-TOF mass spectrometer delivers outstanding performance in a compact footprint, making it an ideal choice for today’s increasingly demanding laboratories.
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Go No Go Testers
Go No Go Testers are developed in portable formats. Typically these are utilized at 'I' Level and 'O' Level test requirements and clear the aircraft LRU for flight.
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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: 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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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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Thermal Testing
At E-Labs, Inc., we support thermal cycling and thermal bakeout vacuum testing requirements. During thermal cycling, the unit experiences repeated heating and cooling as it would when exposed to the harsh environment of space. During thermal bakeout, flight equipment is subjected to an outgassing reduction process so as to decrease the chance of molecular contamination of the spacecraft instrumentation.
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Bus Analyzer
Goebelyzer
Our Goebelyzer analyzer systems offer unparalleled insight into bus data and are used in flight test, system simulation, LRU design, verification and manufacturing test. Supported Interfaces Arinc 664, ASCB-D, Honeywell Flight Controls P2P, Arinc 429, CAN2.0b, Mil Std 1553, RS 422 SDLC/Async, ADC
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Matrix-Assisted Laser Desorption/Ionization Time-of-Flight Mass Spectrometer
AXIMA Confidence
Powerful MALDI-TOF performance for reliable mass information and MS/MS derived structural detail.
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SSFDR Software Integration Rig
MS 1112
Software Integration Rig (SIR) is an Industrial PC based system is used to test the SSFDR (Solid State Flight Data Recorder) of SU30 Aircraft. SIR is a PXI based test platform and it is used to test independent and integrated software tests of the SSFDR.
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Rugged Field Test Set
MTS-207
The MTS-207 is a state-of-the-art portable PXI platform for field testing and data acquisition systems. Its proven architecture has been deployed worldwide on multiple programs including the MTS-206 Maverick Missile system flight line tester, the MTS-209 Common Armament Test Set, the AN/TSM-205B Hellfire System test Set, and many more. It combines the capabilities of the versatile and powerful PXI architecture in a compact, ultra-rugged, flightline qualified enclosure. The MTS-207 is ideal for test and data acquisition applications requiring operation under harsh environmental conditions including flightline, back-shop, or airborne applications.
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ARINC 429 Test & Simulation Interface for PCI
PCI-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/FilteringIRIG-B time code encoder/decoder with free-wheeling modeApplication Interface supporting C/C++, C# and VB.NET Development - Device driver support: Windows, Linux (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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4x 3U OpenVPX MOSA Flight Control Computer
SIU34-FCCVARM-01
SIU34-FCCVARM-01 is a Modular Open Systems Approach (MOSA) DO-178C & DO-254 Certifiable Flight Control Computer (FCC) with low power high performance OpenVPX Xilinx UltraScale+ SBC with Quad Core ARM Cortex -A53, 8 GB DDR4 SDRAM, 32 GB SATA Flash, 2 x 10/100/1000Base-T Ethernet, USB 3.0, FIPS-140-3 Level 3 Cyber Security, and Single Event Upset support.
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Gratings for Scientific Research
HORIBA Scientific’s diffraction gratings are found in cutting-edge scientific applications including ultrafast and highenergy lasers, space flight instruments, astronomy, and synchrotron spectrometers.HORIBA’s scientific gratings are either masters or replicas, depending on the application. HORIBA Scientific also produces custom diffraction gratings, which can be specified according to our customers’ unique technical requirements.
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Intuitive Indoor Inspection
ELIOS 2
Get the job done! Elios 2 intuitive flight experience makes anyone feel like a seasoned pilot from the first flight. Perform flawless inspections with an effective and user-friendly tool, deployed within minutes.
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Force Sensors
TE Connectivity (TE) designs and manufactures force sensors for applications that require high performance or unique packaging, including electro-mechanical flight control, test and measurement and ultra-low cost OEM load cells for medium to high volumes. Based on our proprietary piezoresistive silicon strain gage (Microfused) technology, our sensors combine durability and long-term stability in extremely low cost packages.
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Dual Vehicle Flight Termination System
Kratos Defense & Security Solutions, Inc.
Kratos developed a 200W Dual Vehicle FTS that was specifically designed for use with Unmanned Aerial Vehicles (UAVs), missile systems, and aerial target drones, and it is currently in operation supporting various mission requirements worldwide.
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Electronic Engine Instruments
Is a flight instrument display system in an aircraft cockpit that displays flight data electronically rather than electromechanically.
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Smart Aircraft System
The Astronics Smart Aircraft System makes that possible. Our patented system enables the immediate, cabin-wide gathering of thousands of data points using sensors & IoT (Internet of Things) technology. The result? You get the insight you need—when you need it. Insight that helps you on every flight. Insight that allows you to improve your operational efficiency, your cabin safety, and your overall passenger experience.
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TOFD Method of Acoustic Control
Time-of-flight diffraction method of acoustic control is a software and hardware suite used for material strength testing based on TOFD method of acoustic control.
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Ultrasonic Gas Flow Sensor
GB Series
Panasonic Industrial Devices Sales Company of America
A compact, dual-function Ultrasonic Gas Flow Sensor that measures gas flow and gas concentration for flow rates from 1 to 25 Liters per minute. This Ultrasonic Gas Flow Sensor uses a unique time-of-flight design with an onboard processor to make highly accurate measurements of both gas flow and concentration. Suitable for use with many gases in an easy to implement format.
