MS14 Military Qualified Splitter - Step Global

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Page 1 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!MS14 Military Qualified SplitterTechnical Product DataFeatures Designed & Manufactured to MilitarySpecifications Amplified & Passive Versions Available Passes GPS, Galileo & GLONASS L1/L2 Excellent Gain FlatnessGain L1 - L2 2 dBDescriptionThe military qualified MS14 GPS splitter is a one-input, four-output GPS device. This product typicallyfinds application where an input from an active GPS roof antenna is split evenly between fourreceiving GPS units. The MS14 can be configured to pass DC from an RF output (J2) to the antennainput port (J1) in order to power an active GPS antenna on that port. The remaining RF outputs (J3,J4, and J5) would feature a 200 Ohm DC load to simulate an antenna DC current draw for anyreceiver connected to that port. Alternatively, the MS14 can be configured with a MIL-STD-704compliant 28 VDC Power Supply that will power the active GPS antenna connected to J1.The MS14 splitter comes with many available options to meet your specific needs. Please call, fax,email (sales@gpssource.com), or visit our website (www.gpssource.com) for further information onproduct options and specifications. This device is designed for military applications and environmentswhere high reliability is required.This device has been designed and/or tested to the following MIL MIL-STD-7047/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Page 2 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!0Electrical Specifications, Operating Temperature -40 to 85 CParameterConditionsFreq. RangeGain-Amplified (Normal)-Amplified (Custom)Loss-PassiveInput SWROutput SWRNoise FigureAmplifiedGain Flatness-Amplified:-Passive:Amp. BalancePhase BalanceGroup Delay FlatnessIsolation-Amp/Pass(Norm)(Gain 10dB)-Amplified (Hi Iso.)(Gain 3dB)Output IP3 (Amplified)Output P1dB (Amplified)DC INDC BlkPass DC-Amplified-PassivePoweredMinAnt – Any Port, Unused Ports - 50 Ω1.2Ant – Any Port, Unused Ports - 50 ΩAs Specified (xdB, 0 to 10dB)Ant-Any Port, Unused Ports - 50 ΩAll Ports 50ΩAll Ports 50ΩAnt-Any Port, Unused Ports – 50 Ω, Gain 10dB9X-16.5Typ10X7.5MaxUnits1.7GHz11X 18.52.0:12.0:1dBdBdB-3dB210.51.01dB L1 - L2 , Ant - Any Port, Unused Ports - 50 Ω J2 – J3 , Ant-Any Port, Unused Ports - 50 ΩPhase (J2 – J3), Ant - Any Port, Unused Ports - 50 Ωτd,max - τd,min , J2 – J1 (Ant)Adjacent Ports Ant - 50ΩOpposite Ports: Ant - 50ΩAdjacent Ports Ant - 50ΩOpposite Ports: Ant - 50ΩAnt-Any Port, Unused Ports - 50 Ω, Gain 10dB,Tone spacing 1 MHzAnt-Any Port, Unused Ports - 50 Ω, Gain 10dB16242731dB18dBm4dBmAny DC Blocked Port with a 200 Ω LoadNon-Powered Configuration, DC Input on J2, J3 orJ4516Powered, Mil. C(Normal & Emergency conditions as defined byMIL-STD-704F)(2)DC out (Powered)Current(Iinternal)Amplified, Powered, Mil. Conn., Ant thru current 75mACurrent Consumption of device, excludes Ant. Cur.Ant/Thru Pass DCCurrent PoweredNon-Powered Configuration, DC Input on J2Powered, Mil. Conn. or Quick Connect OptionMax RF Input-Amplified-PassiveMax RF input without damage7/19/2011Document number: 059-FSA-AAA-AAY-AG5452040Rev. 006dBm

Page 3 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!Notes:1. By design 1275B spike & surge protection assumes a 28 volt system, 33.3 V or greater willtrigger over voltage protection circuitry.2. DC output voltage to the antenna port (J1) may be specified by customer: 5V, 7.5V or 9V(default is 5V).3. Available power connector options.Pin A PositivePin B GNDAvailable with options:-PM/XX-PM-1275/XX-PMS-704/XXPin A PositivePin B GNDPin C NCAvailable with XXGeneral SpecificationsWeightThe weight of MS14 is .624 pounds (283 grams)MTBFMean Time Between Failure (MTBF) for GPS Source’s 1x4 (MS14) military spec splitter (Passiveconfiguration) is 367,456 hours at 29 C and 332,884 hrs at 71 C.7/19/2011Document number: 059-FSA-AAA-AAY-AG Rev. 006

Page 4 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!Environmental SpecificationsTemperature and AltitudeThe MS14 complies with the temperature-altitude tests per MIL-STD-810C, Method 504, andCategory 5.Explosive AtmosphereThe MS14 is designed for operation in the presence of explosive mixtures of air and jet fuel withoutcausing explosion or fire at atmospheric pressures corresponding to altitudes from 1,800 feet to50,000 feet The MS14 does not produce surface temperatures or heat in excess of 400 F. The MS14does not produce electrical discharges at an energy level sufficient to ignite the explosive mixturewhen the equipment is turned on or off or operated. The MS14 is designed to meet the requirementsof MIL-STD-810C, Method 511.1, and Procedure II. Hermetically sealed equipment meeting theRequirements of MIL-STD-202, Method 112D, or MIL-STD-883, Method 1014.7 (as applicable), andnot exceeding a Helium leakage rate of 1 x 10-7 cc/sec, are exempt from this requirement.Salt FogThe MS14 meets the requirements of Salt Fog conditions per Paragraph 3.2.24.9 of MIL-E-5400. TheMS14 can withstand a salt concentration of 5 percent at a temperature of 35o C for 48 hours withoutdegradation.FungusThe MS14 meets the requirements of Fungus conditions per Paragraph 3.2.24.8 of MIL-E-5400 i.e.fungus inert materials per requirement 4 of MIL-HDBK-454. MS14 can withstand exposure to 95%relative humidity at a temperature of 30o C for 28 days.HumidityThe MS14 is capable of meeting the requirements of a ten-day humidity test conducted per MIL-STD810C, Method 507.1, Procedure I.Sand & DustThe MS14 meet be capable of meeting the requirements of Sand and Dust conditions of method 510of MIL-STD-810C, for a temperature of 145 F for duration of 22 hours.VibrationThe MS14 is designed to meet the requirements of random vibration per conditions (MIL-STD-810C,Method 514.2, and Procedure 1A) to the levels defined below. Acceleration power spectral density(PSD) for the random vibration envelope is shown in Figure 1. Amplitudes for the functional levelsand endurance level requirements are as shown in Figure 1.7/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Page 5 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!Figure 17/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Page 6 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!ShockThe MS14 is designed to withstand the shock levels specified in the Shock spectrum of Figure 3. andthe saw tooth shock pulse parameter specified in Figure 2.Figure 27/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Page 7 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!Figure 37/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Page 8 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!DecompressionThe MS14 is designed to meet the performance standards during and following a rapid and completeloss of normal cabin compartment pressurization (10,000 ft.) from an airplane flight altitude of 50,000feet within 15 seconds. The MS14 will remain operating for 5 minutes at 50,000 feet before beingreturned to normal cabin pressure.OverpressureMS14 is capable of withstanding, for 3 minutes, while not operating, a 12.1 psi compartment pressurewith no physical distortion or permanent set. The MS14 will operate satisfactorily upon return tonormal pressure.Temperature ShockThe MS14 will withstand without degradation (while not operating) Method 503.1, Procedure I of MILSTD-810C.FlammabilityThe MS14 is self-extinguishing or nonflammable and meets the Requirements of Paragraph 5.2.4 ofMIL-STD-1587 and requirement 3 of MIL-HDBK-454.Finish and ColorsAll case surfaces of the MS14 is treated with chemical film per MIL-DTL-5441, TYPE II, CLASS 3.The MS14 bottom contact surface is free of paint, or non-conductive finishes. The MS14 bottomcontact surfaces are protected from corrosion by a conductive coating (MIL-DTL-5541).All othersurfaces, except connector mating surfaces are primed per MIL-PRF-23377, TYPE 1 CLASS C andpainted per MIL-PRF-85285, TYPE 1 COLOR NUMBER ( 26231), military gray (not lusterless variety)per FED-STD-595 (exceptions are bottom and connector surfaces are free of paint).Human FactorsHuman Engineering principles and criteria (including considerations for human capabilities andlimitations) using MIL-STD-1472 in all phases of design, development, testing, and proceduresdevelopment. The design is free of all sharp edges, according to MIL-STD-1472.7/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Page 9 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!Electromagnetic Interference and Compatibility TestElectromagnetic compatibility requires that the GPS MS14 perform its intended function and that itsoperation does not degrade the performance of other equipment or subsystems. The following tabledefines the test requirements and test procedures for conducting the required electromagneticcompatibility testing.The MS14 is designed to meet the following requirements of 15CS116RE102RS103DescriptionConducted Emissions, Power Leads, 10 kHz to 10 MHzConducted Emissions, Antenna Terminal, 10 kHz to 40 GHzConducted Susceptibility, Power Leads, 30 Hz to 150 kHzConducted Susceptibility, Antenna Port, Intermodulation, 15 kHz to10 GHzConducted Susceptibility, Antenna Port, Cross-Modulation, 30 Hz to 20 GHzConducted Susceptibility, Bulk Cable Injection, 10 kHz to 200 MHzConducted Susceptibility, Bulk Cable Injection, Impulse ExcitationConducted Susceptibility, Damped Sinusoidal Transients, Cables and PowerLeads, 10 kHz to 100 MHzRadiated Emissions, Electric Field, 10 kHz to 18 GHzRadiated Susceptibility, Electric Field, 2 MHz to 40 GHzElectrical Power Service ConditionsThe MS14 is able to accommodate the 28 VDC aircraft power. Consequently, it must perform itsintended function when supplied with the Normal, Emergency and Starting Operation types ofelectrical power defined by MIL-STD-704F. The transfer operation, as defined by MIL-STD-704F,shall not change the operating mode or damage the MS14.The MS14 is designed to meet the following test requirements of MIL-STD-704F:ParagraphMIL-STD-704F, 5.3.2MIL-STD-704F, 5.3.2.1MIL-STD-704F, 5.3.2.2MIL-STD-704F, 5.3.2.3&5.3.2.47/19/2011DescriptionDC Full Performance Characteristics, 28 VDC systemNormal OperationAbnormal OperationDC Steady State Voltage in the Emergency or Starting OperationDocument number: 059-FSA-AAA-AAY-AGRev. 006

Page 10 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!Performance Data:MS14 – PassiveFigure 4. Gain vs. Frequency for Passive MS14 SplitterFigure 5. SWR vs. Frequency Plot for Passive MS14 Splitter7/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Page 11 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!MS14 – ActiveFigure 6. Gain vs. Frequency Plot for Active MS14 SplitterFigure 7. SWR vs. Frequency Plot for Active MS14 Splitter7/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Page 12 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!Available Options:Power Supply Options:Source Voltage OptionsVoltage InputDC 16-28 VDCOutput Voltage Options(1)TypeMilitary Style ConnectorDC Voltage Out57.59RF Connector Options:Connector OptionsNSMATNCConnector ionsPort Options:Pass DC(1)DC Blocked(1)All Ports Pass DCJ3,J4,J5 is DC Blocked & 200Ω Load, DC is passed J2 toANT(J1)More Notes:1. With source voltage option, any or all RF ports (input or output) can be DC Blocked or can passthe powered DC voltage7/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Page 13 of 14Your source for quality GNSS Networking Solutions and Design Services, Now!Part Number:MS14 – A – PMS / 5 – SFProduct:Military Qualified1x4 Splitter(Pass DC J2-Ant (J1), Block DC- J3, J4, J5)Gain Option:A – AmplifiedAS – Amplified Custom Gain by PortAXX – Custom Gain (XXdB)Blank – PassiveSource Voltage:PM – Military Connector (User supplies DC)PMS-1275 – Military Connector (User supplies DC& 1275B Compliant)PMS-704 – Military Connector (User supplies DC& 704F CompliantPM38999 – Military 38999 ConnectorPM38999-1275 - Military 38999 Connector& 1275B CompliantPMS38999-704 – Military 38999 Connector& 704F CompliantBlank – Pass DC J2-Ant (J1), Block DC-J3Output Voltage:5, 7.5, 9VConnector Options:NF – N, FemaleSF – SMA, FemaleTF – TNC, FemaleNM – N, MaleSM – SMA, MaleTM – TNC, Male7/19/2011Document number: 059-FSA-AAA-AAY-AGRev. 006

Your source for quality GNSS Networking Solutions and Design Services, Now!Page 14 of 14For help in creating the part number to meet your exact needs, contact us atSales@gpssource.com or visit our website at www.gpssource.com.Mechanical:ABCD1 FO 1T E EH S1S B L 5.SSA M1: 1N O I TC EJ OR P E LGN A DR 3TUO 4 N I 1 ASF ,41S CEPS L IM.EMAN ELIF SSPGGA-YAA-AAA-AS F-130ELACSCEZISNOITPIRCSED4991 - M5.41 Y EMS A W AISEHCNI NI ERA SNOISNEMIDDEIFICEPS ESIWREHTO SSELNUDEVORPPAGFMSNIKWAD DA VE N E G SETADETADNAOLS N01-30-20D E KC EHCAQ01-30-20NW ARDENOTS G R100ETADETAD01-30-20ENOZETADESAELER NOITCUDORPA10001-40-2001-40-20ESAELER LAITINIV ER100ecruoS SPGEMAN YN APMOC.EC R UOS SPG FO T NESNO C NET TI RW SSE RPXE E H T T UO H TIW NE DDIB ROF SI NGISE D FO NOI T ROP Y NA FONOI T UBIR TSI D RO NOI TC U DORPE R .Y NAP MO C DIAS RO F YLEVIS UL CXE DEV RESER SI NGISE D SIH T FO ES U.E CR UOS SPG FO Y T REPO RP ELOS E H T SI TES NGISE D SI H T NI DE NIAT NO C NOI TA MRO F NI E H TDSDETAD01-40-20V ERDSDNOITPIRCSEDDEVORPPASNOISIVER12R AENILHSINIF1. X.10. XX.500. XXX.5000. XXXX.LAIRETAMYARG SSOLG-IMESMO B E E SRAENIL EESIIDARR ALUGN A1 DEIFICEPS ESIWREHTO SSELNUSECNARELOT2GA-YAA-AAA-AS FREBMUN TR AP ECRUOS SPG3)NWOHS SROTCENNOC )F(EPYT-N(SNOITPO ROTCENNOC LAIXAOC ROFTSIL NOITPO TCUDORP EES92.189.3271. n X4SNOITPO ROTCENNOC REWOP ROFTSIL NOITPO TCUDORP EES3516.3052.3058.260.101.14Rev. 006Document number: 059-FSA-AAA-AAY-AG47/19/2011002.051.236. X6005.2571.

MIL-STD-1472 MIL-HDBK-454 MIL-STD-202 MIL-STD-1587 MIL-STD-883 MIL-STD-461 MIL-STD-704 . Page 2 of 14 Your source for quality GNSS Networking Solutions and Design Services, Now! 7/19/2011 Document number: 059-FSA-AAA-AAY-AG Rev. 006 Electrical Specifications, Operating Temperature - 40 to 85 0 C . Parameter.

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