CINEMA (CubeSat for Ions, Neutrals, Electrons & MAgnetic fields) Jerry Kim * David Glaser † Thomas Immel ‡ * Systems Engineer, †

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Presentation transcript:

CINEMA (CubeSat for Ions, Neutrals, Electrons & MAgnetic fields) Jerry Kim * David Glaser † Thomas Immel ‡ * Systems Engineer, † Lead Mechanical Engineer, ‡ Project Manager, STEIN (SupraThermal Electrons, Ions, Neutrals) IntroProgress Heritage: STEREO STE Sensor With Electrostatic Deflection Mechanical Attenuator Reduces Particle Count by 10 2 Trajectories: Low Energy Electrons Neutrals, High Energy Electrons and Ions Low Energy Ions Development ETU Vibe Test Flight Model Design: In Progress Fabrication: In Progress MAGIC (MAGnetometer from Imperial College) IntroProgress Magnetoresistive Technology Inboard + Boom Deployed Calibration Spacecraft Induce Field Measurement Sensitivity: 0.25 nT Resolution Science Mode (200 mW) 2 to 10 nT ACS Mode (~100 mW) 25 nT Development ETU Single Axis: Complete 3-Axis: In Progress Flight Model Design: In Progress Fabrication: In Progress Uplink: UHF (Ultra High Frequency) IntroProgress Comprised of: (1) Kantronics TNC (1) Custom-designed UHF Whip Antenna (1) Astrodev Helium-100 Radio (1) UMCC PD S Power Splitter RG/316 Coaxial Cable Development ETU Complete Flight Model Design: In Progress Fabrication: In Progress Downlink: S-Band IntroProgress Comprised of: (1) Emhiser S-Band Transmitter (1) ATM P213HT Power Splitter (2) Custom-designed Patch Antennas RG/316 Coaxial Cable Development ETU Complete Flight Model Design: In Progress Fabrication: In Progress Power System IntroProgress Comprised of: (10) Custom-designed Solar Panels (24) TASC Cells (1) Clyde Space Linear EPS (1) Clyde Space 3U Battery Development Solar Panel ETU Vibe Test TVAC (-60 to +94˚C) Flight Model Design: In Progress Fabrication: In Progress Avionics Stack IntroProgress Comprised of: (7) PCBs (4) M3 AISI 316 Threaded Rods (32) 6 mm Diameter Tubular Unthreaded Spacers (8) Custom-designed Stack Center Brackets (1) Remove-Before-Flight (RBF) Bracket (12) M3 Nuts Development ETU Complete Flight Model Design: In Progress Fabrication: In Progress FSW (Flight SoftWare) IntroProgress Foreground Tasks Run async. in available time No hard limit on exec. time Configurable by gnd cmds Freq. interrupt by BKG tasks Background (BKG) Tasks Interrupts 1024 Hz Run at specific times Must complete before next interrupt (~9700 instructions) Development: Completed & Tested: BKG module EPS Module In Progress: SD Card Drivers Transmission Module Future: Final Review of CTM Verification of Software with Hardware GSEOS (Ground Support Equipment Operating System) IntroProgress GSEOS Integration/Test Software for Small Satellites GUI (Graphic User Interface) Supports Python Language Tasks Data Transmission Communication Network with Other Subsystems Store Telemetry Development Transmission Complete Network: In Progress Storage: In Progress Integration Test FSW: In Progress Radio: TBD ACS (Attitude Control System) IntroProgress Comprised of: ACS Software (2) Torque Coils (2) Sun Sensors (1) Magnetometer Development ETU Complete Flight Model Design: In Progress Fabrication: In Progress ACS FSW Integration: In Progress Helium Cmds Analogs I II IVIII Simulink PWR.A ACS.A Sun Sensors Sun Sensors Torque Coils Torque Coils STEIN Atten STEIN Atten MAG Elect MAG Elect STEIN Elect STEIN Elect MAG.A STEIN.A SPI S-Band Tx S-Band Tx TM.A SDCARD STEIN FPGA POWER Switches Timers MAG FPGA BKG.A EXEC.A SSR.A LD.A CMD.A SRAM & EEPROM SRAM & EEPROM HSK.A COMM FPGA FSW MAJOR MODULES SPI Motherboard Sun Sensors Torque Coil S-Band Splitter Emhiser Transmitter Patch Antenna Linear EPS3U Battery Helium Radio Kantronics TNC UHF Splitter Linear EPS 3U Battery Helium Radio IIB MAGIC HVPS