PDS_VERSION_ID = PDS3 RECORD_TYPE = STREAM INSTRUMENT_HOST_NAME = "ROSETTA-ORBITER" OBJECT = TEXT PUBLICATION_DATE = 2018-11-15 INTERCHANGE_FORMAT = ASCII NOTE = " ASCII description of contents of this RPC-MAG Archive" END_OBJECT = TEXT END ************ File AAREADME.TXT ****************** Acronyms: ========== A/D: Analog/Digital A/R: As Required AAD: Attitude Anomaly Detector AC: Alternate Current ACID: Application Configuration Interface Data ACK: Acknowledge ACM: Active Cruise Mode ACS: Avionics Computer System ACS: Attitude Control System ACU: Attitude Control Unit AD: Applicable Document ADC: Analog-Digital-Converter ADD: Architectural Design Document ADP: Acceptance Data Package AFM: Asteroid Flyby Mode AIT: Assembly Integration Tests AIU: AOCMS Interface Unit AIV: Assembly, Integration and Verification ALICE: ORBITER PAYLOAD INSTRUMENT ALS: Alenia Spazio AM: Activation Mode AME: Absolute Measurement Error AND: Alphanumeric Display ANSI: American National Standards Institute AO: Announcement of Opportunity AOCMS: Attitude & Orbit Control Measurement System AOCS: Attitude and Orbit Control System AOS: Acquisition Of Signal AOU: Astronomical Observatory Uppsala APC: Active Payload Checkout APD: Active Payload Data Dump APE: Absolute Pointing Error APID: Application Process Identifier APM: Antenna Pointing Mechanism APXS: LANDER PAYLOAD INSTRUMENT AQP: Acquisition Period AS: Address State (1750 Processor) ASA: Austrian Space Agency ASAP: As soon as possible ASF: Additional Safety Factors ASI: Agenzia Spaziale Italiana ASIC: Application Specific Integrated Circuit ATA: Alignment Test Adapter ATP: Approach Transition Point AU: Astronomical Unit AWG: American Wire Gauge BB: Broad Band BC: Bus Controller BCP1: Broadcast Command Pulse BCU: Battery Charge Unit BDR: Battery Discharge Regulator BDU: Battery Discharge Unit BER: Bit Error Rate B-FIELD: Magnetic Field BFL: Back Focal Length BIT: Build In Test BL: Block Length, LAP BMOS: Buckling Margin Of Safety BOB: Break Out Box BOL: Beginning of Life BPS: Bits per second BRU: Battery Regulator Unit, Battery Recharge Unit BSM: Bus Support Module C/C: Collectively Controlled CA: Contract Authorisation CADU: Channel Access Data Unit CAP: Comet Acquisition Point CAPS: Cassini Plasma Spectrometer CAV: Command Acceptance Verification CC: Cost Code CCB: Configuration Control Board CCCS: Common Checkout & Control System CCD: Charged Coupled Device CCDB: Configuration Control Database CCE: Central Checkout Equipment CCITT: Consultative Committee International Telegraph & Telephone CCN: Change Contract Notice CCR: Configuration Control Request CCS: Central Check-out System CCSDS: Consultative Committee for Space Data Systems CCU: Central Computing Unit CDC: Clock Drift Correction CDMS: Central Data Management System CDMU: Central Data Management Unit CDR: Critical Design Review CDV: Command Dispatch Verification CE: Conducted Emission CESR: Centre d'Etude Spatiale des Rayonnements CEV: Command Execution Verification CFRP: Carbon Fibre Reinforced Plastic CG: 67P/Churyumov-Gerasimenko CGSE: Cryocooling Ground Support Equipment CHF: Critical History File CHL: Command History Log CHM: Critical Housekeeping Unit CI: Configuration Item CIA: Communication Interface Adapter CIDL: Configuration Item Data List CISAS: Centro Interdipartimentale di Studi e Attiviti Spaziali CIVA: Comet nucleus Infrared and Visibility Analyser (Lander Payload) CLA: Calibration level A, data in URF coordinates CLB: Calibration level B, data in S/C coordinates CLC: Calibration level C, data in celestial coordinates CLCW: Command Link Control Word CLE: Calibration level E, resampled data in URF coordinates CLF: Calibration level F, resampled data in S/C coordinates CLG: Calibration level G, resampled data in celestial coordinates CLH: Calibration level H, RW disturbance eliminated data in celestial coordinates CLTU: Command Link Transmission Unit CM: Configuration Management CMD: Command CMF: Configuration Management Facility CMO: Configuration Management Officer CMP: Configuration Management Plan CNES: Centre Nationale d'Etude Spatiale COB: Consolidated Obeservation Request COG: Centre Of Gravity Co-I: Co-Investigator COM: Centre Of Mass CONSERT: ORBITER & LANDER PAYLOAD INSTRUMENTs COP: Command Operations Procedure COSAC: LANDER PAYLOAD INSTRUMENT COSIMA: ORBITER PAYLOAD INSTRUMENT COTS: Commercial Off The Shelf CPDU: Command Pulse Distribution Unit CPU: Central Processing Unit CR: Compression Ratio CRAF: Comet Rendezvous and Asteroid Fly-by mission CRB: CCD Readout Board CRC: cyclic redundancy check CRF: Command Request Files CRID: Command Request Interface Document CReMA: Consolidated Report on Mission Analysis CRP: Contingency Recovery Procedure CRV: Command Station Reception Verification CS: Checksum CS: Conducted Susceptibility CSEQ: Comet-Centric-Solar-Equatorial Coordinates CSG: Centre Spatiale Guyanaise CSM: Communication Switching Matrix CSME: Communication Switching Matrix Element CSP: Charge Sensitive Preamplifier CSPL: Consolidated Parameter Scenario List CSV: Command Station Radiation Verification CSY: Converter Synchronisation CTC: Cost to Completion CUC: CCSDS Unsegmented Time Code CuL: Kupferlackdraht, Enamelled copper wire CUV: Command Uplink Verification CVP: Commissioning and Verification Phase D&D: Design and Development D/L: Down Link D/TOS: Directorate of Technical and Operational Support DARA: Deutsche Agentur fuer Raumfahrtangelegenheiten DAT: Digital Analog Tape DAWG: Data Archiving Working Group DB: Database DBMS: Data Base Management System DC: Data Centre DC: Direct Current DCA: Dedicated Control Area DCL: Declared Components List DCR: Document Change Request DCR: Data Change Request DCR: Dedicated Control Room DCS: Dust Collector Subsystem (COSIMA) DCT: Discrete Cosine Transform DDD: Detailed Design Document DDID: Data Delivery Interface Document DDS: Data Distribution System DDV: Design Development and Verification DEF: Deflector DFMS: Double Focusing Mass Spectrometer DIB: DPU Interface Board DISR: Descent Imager/Spectral Radiometer DLR: Deutsche Zentrum fuer Luft und Raumfahrt e.V. DM: Dynamic Model DMA: Direct Memory Access DML: Declared Materials List DML: Delayed Memory Load command DMPL: Declared Mechanical Parts List DMS: Data Management System DMSS: Distributed Mission Support System DoD: Depth of Discharge DOF: Degree Of Freedom DOP: Division Operating Procedures DOR: Direct Operation Request DPL: Declared Process List DPSS: Data Packet Switching System DPU: Digital Processing Unit DQE: Detector Quantum Efficiency DRAM: Dynamic Random Access Memory DRB: Delivery Review Board DS: Digital Serial Aquisition DS-1: NASA's Deepspace 1 Mission DSDB: Data Sheet Database DSN: Deep Space Network DSP: Digital Signal Processor DSS: Dornier Space Systems DST: Deep Space Transponder DTMM: Detailed Thermal Mathematical Model DVAL: ESA software to check PDS compliant datasets DVALNG: DVAL Next Generation DWG: Drawing DWT: Discrete Wavelet Transform EAICD: Experimenter to Archive Interface Control Document ECDR: Experiment Critical Design Review ECF: Expedited Command File ECLIPJ2000: Ecliptic J2000 Reference Frame ECP: Executable Control Procedures ECR: Expedite Command Request ECR: Engineering Change Request EDAC: Error Detection And Correction EDC: Error Detection Correction EDF: Experiment Description File E-DSF: Expedite - Detailed Schedule File EE: External Entity (SCOE) EEPROM: Electrically Erasable Programmable Read Only Memory EFDR: Experiment Final Design Review EFOR: Experiment Flight Operations Review EGSE: Electrical Ground Support Equipment EID: Event ID EID: Experiment Interface Document EID: Event Identification EID-A: Experiment Interface Document ,Part A EID-B: Experiment Interface Document ,Part B EIDR: Experiment Intermediate Design Review EIRP: Equivalent Isotropic Radiated Power ELC: Electron EM: Engineering Model EMC: ElectroMagnetic Compatibility EMI: ElectroMagnetic Interference EOC: End of Cycle EOL: End of Life EOM: End of Mission EOP: End of Packet EPC: Electrical Power Conditioner EPS: Electrical Power Subsystem EPS: Experiment Planning System EQM: Electrical Qualification Model ERF: Event Reporting Function ERT: Earth Received Time ESA: European Space Agency ESA: Electrostatic Analyzer ESAC: European Space Astronomy Centre ESANET: European Space Agency's communications Network ESARAD: ESA RADiation ESATAN: ESA Thermal Analyser ESD: Electrostatic Discharge ESDS: Electrostatic Discharge Sensitive ESM: Earth Strobing Mode ESOC: European Space Operations Centre ESS: Electrical Support System ESTEC: European Space Research and Technology Centre ESTRACK: European Space Tracking Network ETS: EMC Test Station EUT: Equipment under Test EUV: Extreme Ultra Violet F/D: Flight Dynamics FAR: Flight Acceptance Review FAT: Factory Acceptance Test FAU: File Assembly Unit FCL: Fold-Back Current Limiter FCP: Flight Control Procedure FCS: Flight Control System FCT: Flight Control Team FCV: Flow Control Valve FD: Flight Dynamics FD: Frequency Domain FDIR: Failure Detection, Isolation and Recovery FDR: Flight Dynamics (Control) Room FDR: Functional Design Review FDR: Flight Dynamics Request FDS: Flight Dynamics System FE: Front End FEC: Front End Controller FEE: Front End Equipment FE-LAN: Front-End Local Area Network FEM: Finite Element Model FF: Full Frame FGM: Fluxgate-Magnetometer FID: Function Identifier FIFO: First In First Out FITO: Fabrication and Test Outline FM: Flight Model FM: File Management FMECA: Failure Mode and Effects and Criticality Analysis FMI: Finnish Meteorological Institute FMS: Failure Management system FMS: File Management System FOD: Flight Operations Director FOP: Flight Operations Plan FOP: Flight Operation Procedure FOV: Field Of View FP: Formal Procedures FPA: Focal Plane Assembly FPGA: Field Programmable Gate Array FRAP: Fine Pointing Accuracy Phase FRR: Flight Readiness Review FS: Flight Spare FSS: First Science Sequence FT: File Transfer FTA: Fault Tree Analysis FTP: File Transfer Protocol FTS: File Transfer System FUSE: Far Ultraviolet Spectrograph Experiment FUV: Far Ultra Violet FWM: Filter Wheel Mechanism G/S: Ground Station GFURD: Ground Facilities User Requirements Document GH: Grand Heading GIADA: Grain Impact Analyser and Dust Accumulator (Orbiter Payload) GLEP: Pointing on Ephemeris Phase Phase with gyroless stellar estimator GMI: Global Mapping Insertion GMT: Greenwich Mean Time GPIB: General Purpose Instrument Bus (IEEE 488-75) GPR: Ground Penetrating Radar GRD: Graphic Display GRM: Ground Reference Model GS: Ground Station GSDR: Ground Segment Design Review GSE: Ground Support Equipment GSEP: Pointing on Ephemeris Phase Phase with Gyro-stellar estimator GSIR: Ground Segment Implementation Review GSIS: Ground Station Interface Specification GSM: Ground Segment Manager GSMP: Ground Segment Management Plan GSOC: German Space Operations Centre GSP: Ground commanded Slew Phase GSRQR: Ground Segment Requirements Review GSRR: Ground Segment Readiness Review GW: Gravitational Waves H/W: Hardware HDBK: Handbook HDR: Hardware Design Review HF: High Frequency HFC: High Frequency Clock HGA: High Gain Antenna HGAPM: HGA Pointing Mechanism HIB: Hibernation HIPPS: Highly Integrated Pluto Payload System HK: Housekeeping HL: High Limit HM: Hibernation Mode HMC: Halley Multicolour Camera HOOD: Hierarchical Object Oriented Design HPA: High Power Amplifier HPC: High Power Command HPCM: HPC Module HPD: High Performance Demodulator HRM: Holddown & Release Mechanism HSD: High Speed Data HTCB: Handling Transport Clamp Band HV: High Voltage HVPS: High Voltage Power Supply I&T: Integration & Testing I/C: Individually Controlled I/F: Interface I/O: Input/Output IAA: Instituto de Astrofisica de Andalucia IABG: Industrieanlagenbetriebsgesellschaft IAS: Institute d'Astrophysique Spatiale IAS-CNR: Istituto di Astrofisica Spaziale/Consiglio Nazionale delle Richerche IB: Inboard I-BOB: Intelligent Break Out Box IC: Imperial College, London ICA: RPC Ion Composition Analyzer ICD: Interface Control Document ID: Identifier IDA: Institut fuer Datenverarbeitungsanlagen IDL: Interactive Data Language IDR: Instrument Design Review IEEE: Institute of Electric and Electronics Engineers IES: RPC Ion and Electron Spectrometer IF: Intermediate Frequency IFEM: Interface Finite Element Model IFOV: Intrinsic Field Of View IGEP: Institut fuer Geophysik und extraterrestrische Physik, TU-Braunschweig IMMM: Interface Mechanical Mathematical Model IMP: Imager for Mars Pathfinder INTA: Instituto Nacional de Tecnica Aerospacial IQR: Internal Quality Report IR: Infra Red IS: Impact Sensor (GIADA) ISO: International Standards Organisation IST: Integrated System Test IT: Integration Test IT: Interruption ITL: Instrument Time Line ITMM: Interface Thermal Mathematical Model ITP: Integration Test Plan ITR: Integration Test Report ITT: Invitation To Tender IUE: Internal Ultraviolet Explorer IWF: Institut fuer Weltraumforschung, Graz JPEG: Joint Photographics Experts Group JPL: Jet Propulsion Laboratory KAL: Keep Alive Line KAU: Kilo Accounting Units KBPS: Kilo-Bits Per Second KFKI: Hungarian Research Institute for Particle and Nuclear Physics KO: Kick Off L: Launch (time) LABVIEW: Graphic S/W for Data analysis and H/W control LAN: Local Area Network LAP: RPC Langmuir Probe Experiment LAS: Laboratoire d'Astronomie Spatiale LCB: Last Chance Bit LCDA: Launcher Coupled Dynamic Analysis LCL: Latching Current Limiter LDL: Long Debye Length (LAP/MIP Mode) LEOP: Launch and Early Orbit Phase LESS: Lander Electrical Support System LET: Linear Energy Transfer LEXAN: Polycarbonate resin thermoplastic LF: Low Frequency LGA: Low Gain Antenna LID: Lander Interface Document LIFO: Last In First Out LIGA: Lithographie, Galvanoformung und Abformung LILT: Low Intensity Low Temperature LISN: Line Impedance Stabilization Network LIT: Listen-In Test LL: Low Limit LM: Launch Mode LMSS: Lander Mechanical Support and Separation systems LNA: Low Noise Amplifier LO: Local Oscillator LOR: Lander Operational Request LOS: Loss Of Signal LOS: Line Of Sight LPCE: Laboratoire de Physique et Chimie de l'Environnement LRR: Launch Readiness Review LSB: Least Significant Bit LSI: Large Scale Integration LTP: Long Term Planning LU: Latch Up LV: Latch Valve LVO: Label Value Object LVPS: Low Voltage Power Supply LW: Launch Window LZ: Lander = SSP M&C: Monitoring and Control MAC: Model Assurance Criterion MACOR: Machinable glas ceramic MACS: Modular Attitude Control System MAG: Fluxgate Magnetometer (RPC) MAP: Multiplexing Access Point MAS: Mission Analysis Section MB: Measurement Block MBS: Micro Balance Sensor (GIADA) MC: Measurement Cycle MCF: Magnetic Coil Facility MCM: Monitoring and Control Module MCM: Multi Chip Module MC-OCF: Master Channel ? Operational Control Field MCP: Micro Channel Plate MCR: Main Control Room MCR: Memory Checksum Request MCRR: Mission Commissioning Results Review MCS: Mission Control System MDR: Memory Dump Request MGA: Medium Gain Antenna MGM: Magnetometer MGSE: Mechanical Ground Support Equipment MIB: Mission Information Base MICD: Mechanical Interface Control Document MID: Memory Identifier MIDAS: ORBITER PAYLOAD INSTRUMENT MINT: Monitoring Interval MIP: RPC Mutual Impedance Probe MIP: Mission Implementation Plan MIP: Mandatory Inspection Points MIRD: Mission Implementation Requirements Document MIRO: Microwave Instrument for the Rosetta Orbiter (Orbiter Payload) ML: Memory Load, Medium Level MLC: Memory Load Command MLI: Multi Layer Insulation MM: Mass Memory MM: Memory Management MMB: Mass Memory Board MMD: Mimic Display MMH: Mono Methyl Hydrazine, (MMH-LTO) MMI: Man Machine Interface MMS: Matra Marconi Space MMU: Memory Management Unit MOC: Mission Operations Centre MOD: Mission Operations Department MOI: Moment Of Inertia MOM: Minutes of Meeting MOP: Mission Operations Phase MOS: Margin Of Safety MOU: Memorandum Of Understanding MPA: Mission Planning Area MPAE: Max Planck Institut fuer Aeronomie MPI: Max Planck Institut MPIK: Max Planck Institut fuer Kernphysik MPP: Multiple Phase Pinning MPPT: Maximum Power Point Tracking MPR: Memory Patch Request MPS: Mission Planning System MPS: Max Planck Institut fuer Sonnensystemforschung MPTS: Multi Purpose Tracking System MRB: Material Review Board MRODE: Magnetsrode Coil Facility, TUBS MRT: Mission Readiness Test MSB: Most Significant Bit MSDR: Mission System Design Review MSP : Master Science Plan MSS: Mechanical Support and Separation system MSSW: Mission Specific Software MST: Mission Simulation Test MTL: Mission Timeline MTP: Mid Term Planning MTTR: Mean Time To Repair MUPUS: Multi Purpose Sensor experiment (Lander Payload) MUSC: Microgravity User Support Centre MUX: Multiplexer N/A: Not Applicable NAC: Narrow Angle Camera NACK: Not Acknowledge NAIF: Navigation and Ancillary Information System of NASA NASA: National Aeronautics and Space Administration NASAPSCN: NASA Private System Communication Network NASTRAN: NASA Structural Analysis Tool NAVCAM: Navigation Camera NB: Narrow Band NC: Non Conformity NCM: Near Comet Mode NCR: Non Conformance Report NCTRS: Network Control and Telemetry Receiver System NDIU: Network Data Interface Unit NDM: Neutral Dynamics Monitor NF: Normal Frequency NI: Nation Instruments NM: Normal Mode NOCC: Network Operations Control Centre (JPL) NRT: Near Real Time NRZ-L: Never Return to Zero-Level NTO: Nitrogen Tetroxide OA: Operational Archive OAP: Off Axis Paraboloid OB: Onboard OB: Outboard OBC: On-Board Computer OBC: On-Board Clock OBCP: On-Board Control Procedure OBDH: On-Board Data Handling OBEM: On-Board Event Monitoring OBR: Observation Request OBS: On-Board Software OBSM: On-Board Software Maintenance OBSW: On-Board Software OBT: On-Board Time OC: Output Code OC: Open Centre OCC: Operations Control Centre OCM: Orbit Correction Manoeuvre OCM: Orbit Control Mode OCXO: Oven Controlled Crystal Oscillator OD: Operations Director OGS: Operations Ground Segment OHP: Observatoire d'Haute Provence OIOR: Orbiter Instrument Operational Request OIP: Orbit Injection Point OM: Operations Manager OMM: Operational Macro Mode OOL: Out Of Limits OPAMP: Operational Amplifier OPI: Orbiter Payload Instrument OPS: Operations ORATOS: Orbit Attitude Operations System ORS: Operation Request Structure OSI: Open System Interconnection OSIRIS: Optical, Spectroscopic and Infrared Remote Imaging System (Orbiter Payload) OU: Open University P/B: Play Back (data from Solid State Recorder) P/L: Payload PA: Product Assurance PAIP: Product Assurance Implementation Plan PALASIM: Parallel Access Large Silicon Memory PC: Project Control PC: Passive Checkout PCA: Pressure Controlled Assembly PCAT: Packet Category PCB: Printed Circuit Board PCE: Power Controller Electronics PCM: Pulse Code Modulation PCM: Power Converter Module PCS: Packet Check Sequence PCU: Power Control Unit PDF: Product Definition File PDL: Pseudo Design Language PDOR: Payload Direct Operation Request PDR: Preliminary Design Review PDS : Planetary Data System PDU: Power Distribution Unit PEM: Project Element Manager PEM: Plasma Environment Monitor PERMALLOY: Nickel Iron magnetic alloy PES: Performance Evaluation System PFC: Parameter Format Code PFM: Proto Flight Model PHD: Project History Documents PI: Principal Investigator PID: Process Identifier PID: Parameter Identifier PIR: Post Integration Review PISA: Principal Investigators Support Area PIU: Plasma Interface Unit (RPC) PKT: Packet PLM: Payload Module PM: Project Manager PM: Processing Module PMD: Propellant Management Device PMIS: Project Management Information System PMP: Part Material and Process PMU: Processor Module Unit POR: Payload Operation Request PPWR: Primary Power PRNU: Pixel Response Non Uniformity PROM: Programmable Read Only Memory PRR: Propellant Refillable Reservoir PS: Pass Schedule PSA: Planetary Science Archive PSF: Point Spread Function PSK: Phase Shift Key PSM: Payload Support Module PSR: Project Support Room PSR: Processor Status Registers PSR: Project Status Review PSRI: Planetary Science Research Institute PSS: Portable Satellite Simulator PSS: Procedures, Specifications and Standards PSS: Programme System Standards PSU: Power Supply Unit PT: Product Tree PT1000: Platinum Thermistor with 1000 Ohm nominal resistance PTC: Parameter Type Code PTR: Pointing Requirement File PTT: Post, Telegraph and Telephone authority PTV: Pre-Transmission Validation PUS: Packet Utilisation Standard PVNC: Pyro Valve Normally Closed PVNO: Pyro Valve Normally Opened QA: Quality Assurance QAE: Quality Assurance Engineer QAM: Quality Assurance Management QAPM: Quality Assurance Procedures Manual QC: Quality Control QPM: Quality Policy Manual QTR: Qualification Test Review R&D: Research & Development R/T: Real Time (system) RAF: Return All Frames RAL: Rutherford Appleton Laboratory RAM: Random Access Memory RAMS: Reliability, Availability, Maintainability and Safety RAW: Data in units of ADC counts in instrument coordinates RBW: Resolution Band Width RC: Responsibility Code RC: Remote Computer RCCCS: Rosetta Common Checkout & Control System RCS: Reaction Control Subsystem RD: Reference Document RDB: Rosetta Database RDDD: Rosetta Database Definition Document RDDS: Rosetta Data Disposition System RDM: Raw Data Medium RDVM: Rendezvous Manoeuvre RE: Radiation Emission RF: Radio Frequency RF S/S: Radio Frequency Subsystem (TT&C S/S) RFC: Request For Change RFC: Radio Frequency Self Compatibility RFD: Request for Deviation RFDU: Radio Frequency Distribution Unit RFI: Radio Frequency Interface RFMU: Radio Frequency Mock-Up RFW: Request For Waiver RH: Radiation Hardened RID: Review Item Discrepancy RIS: Remote Imaging System RISC: Reduced Instruction Set Computer RL: Register Load RLA: Register Load Address RLG: Ring Laser Gyro RLGS: Rosetta Lander Ground Segment RM: Reconfiguration Module RMCS: Rosetta Mission Control System RMOC: Rosetta Mission Operations Centre RNCTRS: Rosetta Network Control & Telemetry Receiver System ROIRD: ROSETTA Operations Interface Requirements Document ROKSY: ROSETTA Knowledge Management System ROLIS: LANDER PAYLOAD INSTRUMENT ROM: Read Only Memory ROMAP: Rosetta Magnetic Field and Plasma experiment (Lander Payload) ROSINA: Rosetta Orbiter Spectrometer for Ion and Neutral Analysis (Orbiter Payload) ROSIS: ROSETTA Spacecraft Interface Simulator RP: Rundown Phase RPC: Rosetta Plasma Consortium (Orbiter Payload) RPC-0: RPC Main Electronics Box RPCMAG: ROSETTA Orbiter Magnetometer RPC-MAG: ROSETTA Orbiter Magnetometer RPE: Relative Pointing Error RPM: Remote Processing Module RPRO: ROSETTA Common Packetized Protocol RRP: Rate Reduction Phase RS: Radiated Susceptibility RSDB: Rosetta System Data Base RSI: Radio Science Investigation (Orbiter Payload) RSOC: Rosetta Science Operations Centre RSS: Root Sum Square RT: Real Time RT: Remote Terminal RTC: Real Time Clock RTM: Reduced Thermal Model RTMM: Reduced Thermal Mathematical Model RTOF: Reflectron Time Of Flight RTU: Remote Terminal Unit RW: Reaction Wheels RWA: Reaction Wheel Assembly RWL: Reaction Wheel RX: Receiver S/A: Solar Array S/C: Spacecraft S/C: Spacecraft S/HM: Safe/Hold Mode S/S: Spacecraft Subsystem S/W: Software SA: Solar Array SAA: Solar Aspect Angle SADM: Solar Array Drive Mechanism SAM: Sun Aquisition Mode SAP: Sun Aquisition Phase SAP: Science Activity Plan SAS: Sun Aquisition Sensor SASW: Standard Application Software SBDL: Standard Balanced Digital Link SCET: Spacecraft Elapsed Time SCL: Spacecraft Control Language SCOE: Spacecraft Check Out Equipment SCP: Sun Capture Phase SDB: Satellite (Spacecraft) Data Base SDD: System Design Document SDE: Software Development Environment SDID: Station Data Interchange Document SDR: System Design Review SE: System Engineer SEL: Single Event Latch-up SEPAC: Space Experiment with Particle Accelerator SESAME: LANDER PAYLOAD INSTRUMENT SEU: Single Event Upset SF: Safety Factor SFDU: Standard Formatted Data Units SFT: System Functional Test SGICD: Space Ground Interface Control Document SGM: Safeguard Memory SGS: Science Ground Segment SI: Silicon SID: Science Mode Identifier SID: Structure Identifier SIM: Simulator SIMSAT: Software Infrastructure for Modelling SATellites SIR: Simulation Room SIS: Spacecraft Information System SIS: Spacecraft Interface Simulator SIV: Software Independent Validation SKM: Sun Keeping Mode SLE: Space Link Extension SLI: Space wire Link I/F SM: Structural Model SMCS: Scalable Multi-Channel Communication Subsystem SMD: Surface Mounted Device SNR: Signal to Noise Ratio SOC: Science Operations Centre SOHO: Solar & Heliospheric Observatory SOM: Spacecraft Operations Manager SOR: Spacecraft Operation Request SOT: Science Operations Team SOW: Statement of Work SOWG: Science operating working group SPACON: Spacecraft Controller SPB: Superpixel Binning SPC: Science Programme Committee SPD: Space Division SPEVAL: Spacecraft Performance Evaluation System SPG: Single Point Ground SPICE: Comprehensive S/W system for Celestial Mechanics by NAIF SPL: Scenario Parameter List SpM: Sin-up Mode SPP: Sun Point Phase SPR: Software Problem Report SPT: Specific Performance Test SPWR: Secondary Power SQA: Terma Space Division Quality Assurance SR: Software Requirements SRD: Software Requirements Document SREM: Standard Radiation Environment Model SRR: Subsystems Requirements Review SSC: Source Sequence Counter SSC: Status Consistency Checking SSD: Space Science Department SSMM: Solid State Mass Memory SSP: Surface Science Package SSPA: Solid State Power Amplifier SSR: Solid State Recorder STC: Station Computer STIL: Irish Space Technology Institute STM: Structural Thermal Model STN: Standard STO: Soyuz Transfer Orbit STP: Short Term Planning STP: System Temperature Point STR: Star Tracker STSP: Solar Terrestrial Science Programme SUM: Software User Manual SuM: Survival Mode SVF: Software Validation Facility SVM: Service Module SVT: System Validation Test SW: Software SWG: Science Working Group SWR: Standing Wave Ratio SWRI: South West Research Institute SWT: Science Working Team TBC: To be confirmed TBD: To be Defined TBI: To be Inserted TBP: Time Broadcast Pulse TBR: To be resolved TBS: To be supplied TBW: To be written TC: Telecommand TC S/S: Thermal Control Subsystem TCDL: Test Configuration Data List TCDP: Tele Command Detail Parameter TCGP: Tele Command Global Parameter TCM: Trajectory Correction Manoeuvre TCP-IP: Transport Protocol-Internet Protocol TCS: Test Control System TCS: Thermal Control Subsystem TCSL: Test Configuration Status List TD: Time Domain TER: Terma Elektronic A.S. TF: Transfer Function TFG: Transfer Frame Generator THA: Transport Handling Adapter TID: Task Identifier TIDE: Thermal Ion Dynamics Explorer TLC: Telecommand TLM: Telemetry TM: Telemetry TM: Technical Manager TM: Telemetry TMM: Thermal Mathematical Model TMP: Telemetry Processing System (within ground station) TOP: Transfer Orbit Phase TR: Tone Ranging TRB: Test Review Board TRP: Temperature Reference Point TRP: Test Report TRP: Temperature Reference Point TRR: Test Readiness Review TRRB: Test Readiness Review Board TS: Time Series TSE: Test Support Equipment TSP: Test Specification TSY: Timer Synchronisation Pulse TT&C: Tracking, Telemetry & Commanding TT&C S/S: Telemetry, Telecommand and Communication Subsystem (RF S/S) TUB: Technical University of Berlin TUB: Technical University Braunschweig TUBS: Technical University Braunschweig TUB: Technical University of Budapest TV: Thermal Vacuum TWTA: Travellling Wave Tube Assembly TWTL: Two Way Travelling Lighttime TX: Transmitter U/L: Up Link UARS: Upper Atmospheric Research satellite UD: User Defined UFT: Unit Functional Test UM: User Manual UMOS: Ultimate Margin Of Safety UPM: Universidad Politecnica de Madrid URD: User Requirements Document URF: Unit Reference Frame us: microsecond USO: Ultra Stable Oscillator UTC: Universal Time Coordinated UTC: Universal Time Code UV: Ultra Violet UVD: Under Voltage Detector UVSC: Ultra Violet Spectrometer Component V&V: Verification & Validation VC: Virtual Channel VCA: Virtual Channel Assembler VCM: Virtual Channel Multiplexer VDC: Voltage Direct Current VDU: Video Display Unit VHDL: VHSIC Hardware Description Language VHF: Very High Frequency VHSIC: Very High Speed Integrated Circuit VI: Virtual Instrument, S/W Routine for NI Labview VIMS: Visual Infrared Mapping Spectrometer VIRTIS: ORBITER PAYLOAD INSTRUMENT VIS: Vertical Integration Stand VIS: Visual VSWR: Voltage Standing Wave Ratio VT: Validation Test VTP: Validation Test Plan VTR: Validation Test Report W/S: Work Station WAC: Wide Angle Camera WAOSS: Wide Angle Optoelectric Stereo Scanner WBS: Work Breakdown Structure WBS: Workpackage Breakdown Structure WCA: Worst Case Analysis WD: Watch Dog WDE: Wheel Drive Electronics WDW: Window WIU: Wave Guide Interface Unit WOL: Wheel Offloading of RW WP: Work Package WPD: Work Package Description WRT: With Respect To WTC: Wavelet Transform Coding WVR: Water Vapor Radiometer WWW: World Wide Web YMOS: Yield Margin Of Safety ZOM: Zero Order Monitor Overview: ========= This data set contains calibrated data obtained by the Fluxgate Magnetometer (RPC-MAG) onboard the ROSETTA spacecraft from the STEINS Flyby Phase (AST1), for the time interval September 1, 2008 until September 10. The real flyby happened at September 5, 2008 at 18:38 at a closest approach distance of about 800 km. The magnetometer consists of two sensors, the OB and the IB sensor, mounted on a spacecraft boom. The instrument provides 3 component magnetic field vector data measured by both sensors. In this data set the calibrated data can be found. Magnetic field data are given in nanotesla. REMARK: Due to strong magnetic disturbance by the ORBITER, the magnetic field data are influenced by s/c generated magnetic fields. The source of these disturbance is manifold: - transient currents flowing on the spacecraft - Heater pulses - Thruster related magnetic field - Reaction wheel signatures - etc. Due to the complexity of these circumstances a proper data cleaning is an ongoing task. Thus the data of the present dataset still contain the mentioned disturbance signatures. For details please refer to the documentation in the CALIBRATION and INTERFERENCE folders of the DOCUMENT directory. Any use of the data for scientific research has to be done under consideration of these manifold disturbances. STEINS FLYBY (AST1) RPC-MAG Data Archive ======================================== a) S/C DATA =========== CODMAC Level/Type Data Type Data Content 3 / CALIBRATED Data table Calibrated TS of OB,IB,HK data The data can be found in the ./DATA/CALIBRATED/2008/SEP directory. This directory has three subdirectories: LEVEL_A LEVEL_B LEVEL_C The LEVEL_A data (HK,IB,OB) are calibrated data in Instrument coordinates. The LEVEL_B data (IB,OB) are calibrated data in S/C coordinates. The LEVEL_C data (IB,OB) are calibrated data in CSEQ coordinates. b) Supporting files ====================== Supporting files for the Archive user include PDS descriptions, documents, and searchable indices. These have been organized into three directories one level below the root: CATALOG,CALIB, DOCUMENT,INDEX. Structure of the volume ======================== AAREADME.TXT (PDS required introduction to the data set) VOLDESC.CAT (PDS required volume description of the data only) ./CATALOG/CATINFO.TXT (list of catalog files) *.CAT (Mission, spacecraft, instrument, data, references) ../CALIB/CALINFO.TXT (list of calib files) *.LBL (PDS Label for *.ASC files RPCMAG_GND_CALIB_FSDPU_FMIB.ASC Ground Calibration Parameter File for Flight SPARE DPU with FM Inboard sensor RPCMAG_GND_CALIB_FSDPU_FMOB.ASC Ground Calibration Parameter File for Flight SPARE DPU with FM Outboard sensor INFCAL_OFF__IB_20180305.ASC Inflight calibration Parameter for IB, Temperature Model INFCAL_OFF__OB_20180305.ASC Inflight calibration Parameter for OB. Temperature Model INFCAL_PARA_IB_20180305.ASC Inflight calibration Parameter for IB, Offset Jumps INFCAL_PARA_OB_20180305.ASC Inflight calibration Parameter for OB, Offset Jumps RPCMAG_SC_ALIGN.ASC Matrices for stowed and deployed MAG boom in relation to s/c coordinates RPCMAG_BOOM_ALIGN_CORR_EF1.ASC Boom Orientation correction angles obtained from EF1 Analysis. ./DOCUMENT/DOCINFO.TXT (list of documents) *.PDF (PDF documents) ./INDEX/INDXINFO.TXT (Description of the contents of the index directory) INDEX.LBL (PDS LABEL file for INDEX.TAB) INDEX.TAB (Index of the data set in tabular format) ./DATA/CALIBRATED/*.TAB (MAG data, 3 components presented as ASCII tables) *.LBL (PDS LABELS of the MAG data files) The ROSETTA project decided that the data would be archived in the PDS format. Consequently, the layout of this volume and the labels for each file conform to the PDS/PSA guidelines. Contact: ======== Data generated by: Dr. Ingo Richter Technical University Braunschweig Institute for Geophysics and Extraterrestrial Physics Mendelssohnstr. 3 38106 Braunschweig Germany i.richter@tu-bs.de RPC-MAG PI: Prof. Dr. Karl-Heinz Glassmeier Technical University Braunschweig Institute for Geophysics and Extraterrestrial Physics Mendelssohnstr. 3 38106 Braunschweig Germany kh.glassmeier@tu-bs.de