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    AVIONICS INSTRUMENTS Search Results

    AVIONICS INSTRUMENTS Result Highlights (5)

    Part ECAD Model Manufacturer Description Download Buy
    BLA1011-2 Rochester Electronics LLC BLA1011-2 - N-Channel LDMOS Avionics LDMOS Transistor (Ampleon Die) Visit Rochester Electronics LLC Buy
    BLA1011-300 Rochester Electronics LLC BLA1011-300 - 300W LDMOS Avionics Power Transistor (Ampleon Die) Visit Rochester Electronics LLC Buy
    BLA1011-10 Rochester Electronics LLC BLA1011-10 - N-Channel LDMOS Avionics LDMOS Transistor (Ampleon Die) Visit Rochester Electronics LLC Buy
    BLA0912-250 Rochester Electronics LLC BLA0912-250 - N-Channel LDMOS Avionics LDMOS Transistor (Ampleon Die) Visit Rochester Electronics LLC Buy
    54HC158/BEA Rochester Electronics LLC Replacement for Texas Instruments part number 5962-8682301EA. Buy from authorized manufacturer Rochester Electronics. Visit Rochester Electronics LLC Buy

    AVIONICS INSTRUMENTS Datasheets Context Search

    Catalog Datasheet MFG & Type PDF Document Tags

    2948B

    Abstract: Avionics
    Text: Avionics Option 25 Avionics option for the 2948B Low Phase Noise Communications Service Monitor Communication and ramp testing of military and commercial aircraft in one instrument • Avionics modes for ILS, VOR, marker beacons and SELCAL • Displays in avionics terms: SDM, DDM,


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    PDF 2948B 2948B Avionics

    arinc 629

    Abstract: DT650-220 ARINC-629 ARINC 629 sim ARINC629 DT650 DT6502 D227W201 ACRS232CBL
    Text: Avionics DT650 ARINC 629 DATABUS ANALYZER Powerful capabilities for avionics maintenance The DT650 ARINC 629 databus analyzer is a powerful tool that can be used on the ramp or on the bench. The DT650 can be configured with up to three independent transceiver channels. Basic receive


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    PDF DT650 RS-232C arinc 629 DT650-220 ARINC-629 ARINC 629 sim ARINC629 DT6502 D227W201 ACRS232CBL

    Crystal oscillator 12 MHz

    Abstract: TFT210 crystal oscillator
    Text: CRYSTAL OSCILLATOR Series 6T, TEMPERATURE COMPENSATED CRYSTAL OSCILLATOR APPLICATION  Mobile communication, Avionics,  Test Equipment, Electronic instruments ELECTRICAL SPECIFICATIONS Items Frequency Range MHz F-T stability (ppm) Operating Temperature


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    PDF TFT210 TFT230 TFT250 TFT270 TFT300 5x12x 25x15x10 30x20x10 Crystal oscillator 12 MHz TFT210 crystal oscillator

    SM320F240HFPM40

    Abstract: 84-CQFP HT gas sensor 172CQFP 7615 ADS1278 OPA211-HT TPS62000-HT tle2022mjgb Texas instruments HiREL
    Text: Harsh Environments Guide Amplifiers Data Converters Digital Signal Processors Interface Microcontrollers Power Management www.ti.com/he 4Q 2009 2 2 ➔ Avionics Harsh Environments Guide Overview Design considerations The Texas Instruments High Reliability


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    Untitled

    Abstract: No abstract text available
    Text: SENSOR PRODUCTS Precision Pressure Transducer APPLICATIONS Avionics Instrumentation and Analytical Equipment PPT Flow and Pressure Calibrators H oneywell’s precision pressure transducer PPT offers extraordinary value with high accuracy over a wide temperature


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    PDF RS-232 RS-485

    ppt 0020 A

    Abstract: GAS SENSOR FREE PPT ppt 0020 d Digital Differential Pressure Gauge ppt 0020 PPT0100AWN2VA-A EN50081-1 EN50082-1 M2002 pressure transducer application
    Text: SENSOR PRODUCTS Precision Pressure Transducer APPLICATIONS Avionics Instrumentation and Analytical Equipment PPT H Flow and Pressure Calibrators oneywell’s precision pressure transducer PPT offers extraordinary value with high accuracy over a wide temperature


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    PDF RS-232 RS-485 ppt 0020 A GAS SENSOR FREE PPT ppt 0020 d Digital Differential Pressure Gauge ppt 0020 PPT0100AWN2VA-A EN50081-1 EN50082-1 M2002 pressure transducer application

    pressure vessel

    Abstract: radiation tolerant ethernet computer nasa Thruster Inertial navigation system
    Text: DragonLab TM Fast track to flight. Overall Dragon TM Capabilities Dragon is a free-flying, reusable spacecraft capable of hosting pressurized and unpressurized payloads. Subsystems include propulsion, power, thermal control, environmental control, avionics, communications, thermal protection, flight


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    ppt on transducers

    Abstract: Digital Differential Pressure Gauge 6 pin connector 6-282-6sg-522 M2002 PPT100-1G-XF-2V-A PPT100-1G-XF-2V-B 0-5V pressure sensor ppt MS3116F10-6S CONECTOR Type F
    Text: SENSOR PRODUCTS Precision Pressure Transducers APPLICATIONS Avionics PPT / PPT-R Instrumentation and Analytical Equipment Flow and Pressure Calibrators H Meteorology oneywell offers extraordinary value with our family of accurate and very competitively priced smart pressure transducers. The PPT couples


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    GAS SENSOR FREE PPT

    Abstract: ppt on transducers 6 pin connector 6-282-6sg-522 mechanical SENSOR FREE PPT 0-5V pressure sensor ppt 6-282-6SG-522 Digital Differential Pressure Gauge Cannon connectors conector cannon MS3116F
    Text: SENSOR PRODUCTS Precision Pressure Transducers APPLICATIONS Avionics PPT / PPT-R Instrumentation and Analytical Equipment Flow and Pressure Calibrators H Meteorology oneywell offers extraordinary value with our family of accurate and very competitively priced smart pressure transducers. The PPT couples


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    IFR2030

    Abstract: set top box RF
    Text: Application Note ILS Monitor Testing The ILS software both controls a 2030 Avionics Signal Generator and displays relevant paragraphs of a Microsoft Word maintenance schedule. For the very latest specifications visit www.aeroflex.com Introduction Major airports throughout the world are equipped with


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    GLOBAL NAVIGATION 3000

    Abstract: Avionics no fault found
    Text: For more information, contact: Tarah Nimz McClenahan Bruer Communications 503 546-1000 tarah@mcbru.com James E. De Broeck Aeroflex Incorporated (316) 522-4981 jim.debroeck@aeroflex.com FOR PRINT AND ONLINE RELEASE: April 14, 2008 Aeroflex Announces Industry’s First Reconfigurable Avionics Test


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    PDF aboutus/pressroom/newsrelease/2008/041408 2008--Aeroflex GLOBAL NAVIGATION 3000 Avionics no fault found

    NE213

    Abstract: BC501 XC4010E scintillator PLCC84 package transistor BC501 A274 A292 PLCC84 XC4010XL
    Text: NEUTRON SINGLE EVENT UPSETS IN SRAM-BASED FPGAs* Mattias Ohlsson Peter Dyreklev Karin Johansson Ericsson Saab Avionics AB Electromagnetic Technology Division 581 88 Linköping, Sweden and Peter Alfke Xilinx, Inc. 2100 Logic Drive, San Jose CA 95124, USA Abstract


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    PDF NE213 BC501 XC4010E scintillator PLCC84 package transistor BC501 A274 A292 PLCC84 XC4010XL

    GLONASS chip

    Abstract: glonass GNS743A-1L-110 GNS-743A K124 GNS743A-2L GNS-743A-2L gps glonass gps/glonass receivers
    Text: Avionics GNS-743A GPS/GLONASS SATELLITE SIMULATOR The answer to RF leakage, calibration and RF controllability problems in receiver test applications • Simulation of any GPS or GLONASS L1 frequency, K=1-24 satellite • Low noise RF output from -158 dBm to


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    PDF GNS-743A GLONASS chip glonass GNS743A-1L-110 K124 GNS743A-2L GNS-743A-2L gps glonass gps/glonass receivers

    Untitled

    Abstract: No abstract text available
    Text: Elgar TrueWave Series 1750–22200 VA Avionics and Commercial Applications 156–312 V 6.5–192 A • IEC Flicker Test Capable • Field Parallel Configurable • 3 phase output from a single unit 208 • Low Harmonic Distortion • DC Output 230 400 230


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    PDF A162000-01

    arinc 629

    Abstract: ARINC 629 sim DT600-00-220 D227W201 ARINC-629 arinc 429 bus analyzer 110v B777 AC20670600 AC206 A330
    Text: Avionics DT600 ARINC 429/629 DATABUS ANALYZER A powerful tool that can be used on the ramp or on the bench The DT600 is a combination ARINC 429/629 databus analyzer with dual, independent ports for each bus standard. Nearly identical functions are provided for each bus type. These


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    PDF DT600 RS-232 arinc 629 ARINC 629 sim DT600-00-220 D227W201 ARINC-629 arinc 429 bus analyzer 110v B777 AC20670600 AC206 A330

    Untitled

    Abstract: No abstract text available
    Text: California Instruments P Series General purpose Bench top AC power sources 800VA1250VA 135–270 V 6–9.2 A • Low THD • Portable Power, Low Cost. • 810 VA to 1250 VA Output Power 115 • Simple Front Panel Operation 230 • 16 Hz to 500 Hz Frequency Range


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    PDF 800VAâ 1250VA 1001P 1251P

    Untitled

    Abstract: No abstract text available
    Text: California Instruments RP Series 800–2000 VA 150–300 V General purpose AC power sources 3–45 A • Portable Power, Low Cost. • 800 VA, 1250 VA and 2000 VA Output Power • Front and Rear Outputs • 16 Hz to 5000 Hz Frequency Range • High Peak Current Capability


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    PDF IEEE-488 RS232C 801RP 1251RP 2001RP 2003RP

    "D-Subminiature Connector" 26 Pin High Density

    Abstract: "D-Subminiature Connector" 62 Pin High Density "D-Subminiature Connector" 78 Pin saver 289-0125H104JFGR "D-Subminiature Connector" 104 Pin High Density Outgassing E-595
    Text: Backshells and Accessories 289-012 Series 28 HiPer-D Sav-Con D-Subminiature Connector Saver Sav-Con® D-Subminiature Connector Saver Prevent damage to expensive instruments and cables with Glenair HiPer-D Sav-Cons®. One side is a pin connector and the other side is a socket connector. Low profile


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    PDF M24308 "D-Subminiature Connector" 26 Pin High Density "D-Subminiature Connector" 62 Pin High Density "D-Subminiature Connector" 78 Pin saver 289-0125H104JFGR "D-Subminiature Connector" 104 Pin High Density Outgassing E-595

    Untitled

    Abstract: No abstract text available
    Text: series 28 HiPer-D Accessories Sav-Con D-subminiature connector saver 289-012 Prevent damage to expensive instruments and cables with Glenair HiPer-D SavCons®. One side is a pin connector and the other side is a socket connector. Low profile one-piece machined aluminum housing and ground spring protect circuits


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    PDF M24308

    rohde UPA audio analyzer

    Abstract: BIT 3251 circuit diagram of MOD 100 counter using ic 7490 am2 SOCKET PIN LAYOUT NAV-750C SERVICE MANUAL oscilloscopes pm 3210 circuit diagram of MOD 8 counter using ic 7490 rohde UPA equivalent des circuit integre ttl amd am2 socket pin diagram
    Text: SIGNAL GENERATOR NAV-750C Operating Manual Document part no. 46892/293 Issue 8 17 May 2007 Operating Manual SIGNAL GENERATOR NAV-750C 10 kHz to 1.35 GHz This manual applies to instruments with software issues of 8.09 and higher. Aeroflex International Ltd. 2007


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    PDF NAV-750C rohde UPA audio analyzer BIT 3251 circuit diagram of MOD 100 counter using ic 7490 am2 SOCKET PIN LAYOUT NAV-750C SERVICE MANUAL oscilloscopes pm 3210 circuit diagram of MOD 8 counter using ic 7490 rohde UPA equivalent des circuit integre ttl amd am2 socket pin diagram

    he804

    Abstract: ati connector HE809 smd diode ED MMSD32032602S-C-xx Microspire MB he807 eurofarad TCN30 MMEE08510804S-C-xx mmfl16016604s-c mmfl16016604s-d
    Text: Edition 1.2. Space- & Military Level Components 2008/08 2 Introduction and Table of Contents If you are working on a program for military, industrial and/or space equipments & need product with extended temperature performance, MSA Components can help. To support the customer needs


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    AM3517 zoom

    Abstract: sgx530 2.4 lcd qvga 320x240 graphics card texas instruments LQ043T1DG01 wqvga LQ64D343 G
    Text: PRODUCT BRIEF: Logic PD : Texas Instruments www.logicpd.com/ti Zoom AM3517 eXperimenter Kit Logic PD’s product-ready software and hardware platforms fast forward your product development while reducing risk and controlling costs. The Zoom AM3517 eXperimenter Kit


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    PDF AM3517 3-WQVGA-10R LQ043T1DG01 4-VGA-10R LQ64D343 480x272 AM3517 zoom sgx530 2.4 lcd qvga 320x240 graphics card texas instruments wqvga LQ64D343 G

    Untitled

    Abstract: No abstract text available
    Text: DB LECTRO Ine CRYSTAL OSCILLATOR TEMPERATURE COMPENSATED CRYSTAL OSCILLATOR- TFT Series APPLICATION • Mobile communication, Avionics, Test Equipment, Electronic instruments _ ELECTRICAL SPECIFICATIONS Items Frequency Range MHz F-T stability (ppm)


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    PDF TFT210 TFT230 TFT250 TFT270 TFT300 50Q/100Q pu5x10 30x20x10 40x25x15 44x27x19

    common mode rejection ratio test 1553B

    Abstract: No abstract text available
    Text: MIL-STD-1553 B A C K G R O U N D IN F O R M A T IO N During the 1950s, military aircraft m ission requirements reached such a level of complexity that they could no longer be satisfied with independent and self-sufficient electronics avionics subsystem s. There was a recog­


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    PDF MIL-STD-1553 1950s, 26/No. common mode rejection ratio test 1553B