Compact Half-Unit IES for CubeSat Operations
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1 Compact Half-Unit IES for CubeSat Operations Joshua Méndez (Boston University) David Voss (AFRL) Francisco Suárez (Boston University) Theodore A. Fritz (Boston University) Doug Carssow (NRL) Avi Gunda (Boston University)
2 Geophysical background - Open and closed geomagnetic field lines - Particles become trapped along closed field lines - electrons; however ion populations of solar wind and ionospheric origin are also present
3 High Latitude Trapping Boundary
4 Scientific goals 1) Develop a better understanding of the motion of the HLTB and its relation to spaceweather activities. 2) Identify how scattering modifies the pitch angles of energetic particles within the HLTB.
5 Compact Half-u IES for Cubesat Operations (CHICO) CHICO AutoDesk CAD -Based on the Loss Cone Imager's (LCI), Fixed Sensor Head (FSH) -CHICO provides the spaceweather community with a low cost, yet powerful instrument, for magnetospheric research
6 Basic Functionality 1) Detect particles in the range of 30 kev and 500 kev 2) Amplify and shape events 3) Digitize shaped events 4) Packetize and time-stamp data
7 Silicon detectors
8 Readout Electronics for Nuclear Applications 3 (RENA3) - The RENA3 is a 36-channel pulse amplification and shaping Application Specific Integrated Circuit (ASIC) - Each channel includes independently configurable gain, integration time and input polarity - The RENA3 was used in the FSH for the LCI instrument
9 RENA3 channel block diagram
10 Instrument Block Diagram
11 Completed IES in housing Telescope 1 Telescope 2
12 Instrument highlights - Mass: ~0.3 kg - Volume: Smaller than 0.5 CubeSat Unit - Power: Less than 2 W (5V, 12V, -12V) - FOV: 120 degrees (180 degrees with appropriate rotation) - Particle energy range: 30 kev to 500 kev - Unit cost: <10k USD
13 Testing - Preliminary instrument testing with Ortec research pulser - Lower detection threshold ~30 kev - Instrument calibrated with internally generated pulse - Future testing will include EU155 sources
14 RENA3 analog stages
15 RENA3 analog output
16 CHICO noise performance - Full-width half maximum (kev) for shown data: 50 kev: kev: kev: kev: 8.46
17 Angular resolution - Three orders of magnitude rejection of scattered electrons when compared to the incident beam - Plot shows counts versus incident angle measured for the LCI FSH
18 Twin Imaging of the Moving Electron boundary (TIME) - Two student-built 1.5 U CubeSats - 8 measurements of the HLBT per orbit - Each CubeSat will fly a small, three-axis magnetometer and a GPS in addition to CHICO - 6-month mission
19 Student Training - TIME draws heavily from Boston University BUSAT program - Aims to institutionalize student training in satellite development at BU
20 CHICO integrated into TIME
21 THANK YOU! AKNOWLEDGEMENTS: Senior Design Team 13 Spaceweathermen: CHICO at the Boston University ECE Day 2011 Masato Nakanishi (Aero. Eng. BU '11) Micheal Lloyd (Physics BU '11) Orin Hall (Mech. Eng. BU '11) Preston Miller (ECE, BU '11) Robert Kingsland (SIF BU) Xiang He (PhD ECE BU '11) Nathan Darling (BUSAT) BUSAT II Team
22 Extra Slides
23 all pitch angle Pitch angle and the loss cone Particles with pitch angles that fall within the red area, called the loss cone, will likely be lost
24 Particle motion Diagram from Walt, 2005
25 Heritage IES IES from Boston University Student-satellite for Applications and Training (BUSAT) IES-Fixed Sensor Head (FSH) from the Loss Cone Imager (LCI) instrument
26 Analog Board - Six layer board - 12 detector pixel inputs - Houses RENA3, 12- bit ADC and lownoise voltage regulators - Complex grounding scheme for noise
27 Digital Board - Houses Xilinx FPGA and flash PROM - USB, UART and differential I2C (following the BUSAT inter-cube communication Space Plug and Play standard)
28 TIME configuration
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