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QB50 System Requirements Document

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3 AbbreviationsADCCEMDACEGSEEMCEMIESDFMMUFPGAHSDRHVI/FIMSkbpsLEOLUTLVLVDSMb/dayMSSLNMSOBCPCBPWMS/CSEESMDSPISUTBCTBDTBIAnalogue to Digital ConverterChannel Electron MultiplierDigital to Analogue ConverterElectronic Ground Support EquipmentElectromagnetic CompatibilityElectromagnetic InterferenceElectro-Static DischargeFlash Mass Memory UnitField Programmable Gate ArrayHigh Speed Data RecorderHigh VoltageInterfaceIon Mass SpectrometerKilo-bits per secondLow Earth OrbitLook Up TableLow VoltageLow Voltage Differential SignallingMega-bit per dayMullard Space Science LaboratoryNeutral Mass SpectrometerCubeSat On-Board ComputerPrinted Circuit BoardPulse Width ModulatorSpacecraftSingle Event EffectsSurface Mount DeviceSerial Peripheral InterfaceScience UnitTo be confirmedTo be decidedTo be included4 Electrical InterfacesThere will be a single electrical connector between a Science Unit (SU) and aThe Science Unit shall provide a 25-way STRAIGHT MDM-female connector for

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