Mil-Std-1760
military aircraft and their stores electrical interconnection system.
See Also: MIL-STD, Mil-Std-1553
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Product
Flight-Certifiable SBC
SBC314C
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The SBC314C flight-certifiable single board computer is engineered in accordance with DO-178C and DO-254 and is available with supporting artifacts. It delivers great and proven performance thanks to the Power Architecture T2081 processor, and its diverse I/O set brings high functionality to the small form factor. The integrated XMC site allows even more connectivity, including high-density MIL-STD-1553 and ARINC 429 data bus communications as well as avionics discrete I/O through our RAR15CX flight-certifiable mezzanine.
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Product
1 Channel, MIL-STD-1553, Dual Redundant, Direct Coupled, Assisted Mode Capable (AMC)
FTD
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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).
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Product
Micro Coax, Contact, Receiver, RG316
610140101
Coax Contact (ITA)
Primary mating contact 610141101. (May mate with other ITA contacts, as well.)Mechanical SpecificationsDurability 10,000 cyclesContact Material Center Conductor – BeCuShield – BrassContact Plating 50µ" Au over 100µ" NiContact Termination Center Conductor - SolderShield - CrimpInsulator PTFEMating Force 1.5 lbs max [0.68 kg]Electrical SpecificationsCharacteristic Impedance 50ΩFrequency Range DC to 3 GHzVSWR 1.22 @ 3 GHzInsertion Loss – √f(GHz) x .06 dBDWV 800 V RMSContact Resistance 6 mOhms center/4 mOhms outerCable Specifications RG316Environmental SpecificationsOperating Temperature -65°C to +125°CVibration MIL-STD 202, Method 204, Test Condition DShock MIL-STD 202, Method 213, Test Condition IInsulation Resistance 2000 MOhms Min.
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Product
High Sensitivity Helium Leak Detection System
HSHLD® MODEL 310
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ORS manufactures the HSHLD® Model 310 High Sensitivity Helium Leak Detection System, a Quadrupole Mass Spectrometer system for High Sensitivity Helium Leak Rate measurement to qualify your product to the latest, tighter leak rate requirements of Mil-Std-883, Method 1014. Our model HSHLD® Model 310 uses conventional mass spectrometer helium leak test technology. This gives you enhanced spectrometer sensitivity at a modest cost. The system is modular, automated, flexible, fast, easy to calibrate, easy to use, and is affordable. Both the FINE and GROSS leak test is performed in a single test sequence.
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Product
MIL-STD-1553 A / B Test And Simulation VME Module
VME-1553
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*Dual redundant*1, 2, 4 or 8 channels*Simultaneous bus controller, 31 remote terminals, bus monitor*Error entry and detection*FPGA based hardware architecture*Multi-level trigger for data acquisition and filtering*10 programmable, discrete I / O*IRIG-B timecode encoder / decoder with free-running mode*Real-time recording and physical bus playback*Supports: C, C ++, C # and .net*VISA based VXI Plug & Play driver*Optional twinax front end
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Product
ARINC-664 Part 7 Test and Simulation Board
EXC-664PCIe
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The EXC-664PCIe board is an ARINC-664 part 7 test and simulation board designed to help integrate avionics suites, and can simulate up to two ARINC-664 P7 End Systems with full dual redundant support for receive and transmit operation. The board also contains room for two standard 4000 modules that can support multiple channels of other avionics communications protocols including MIL-STD-1553, ARINC-429, Serial, Discrete, ARINC-708 and CANbus.
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Product
MIL-STD-1553 XMC Interface Module
XMC-1553
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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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Product
Avionics System Power
58WS1-03
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- 3Ø AC input per MIL-STD-704A- 1,500 Watts continuous, 3,000 Watts peak power- Environmentally sealed ATR style case- Continuous Background Built-In-Test (BIT) and ETI- EMI compliance
