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Design,Development, Implementation,and On-orbit Performance of the Dynamic Ionosphere CubeSat Experiment Mission |
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| Authors: | C. S. Fish C. M. Swenson G. Crowley A. Barjatya T. Neilsen J. Gunther I. Azeem M. Pilinski R. Wilder D. Allen M. Anderson B. Bingham K. Bradford S. Burr R. Burt B. Byers J. Cook K. Davis C. Frazier S. Grover G. Hansen S. Jensen R. LeBaron J. Martineau J. Miller J. Nelsen W. Nelson P. Patterson E. Stromberg J. Tran S. Wassom C. Weston M. Whiteley Q. Young J. Petersen S. Schaire C. R. Davis M. Bokaie R. Fullmer R. Baktur J. Sojka M. Cousins |
| Affiliation: | 1. Space Dynamics Laboratory, Utah State University Research Foundation, 1695 North Research Park Way, North Logan, UT, 84341, USA 2. Center for Space Engineering, Utah State University, Logan, UT, USA 3. Electrical and Computer Engineering Department, Virginia Tech, Blacksburg, VA, USA 4. Utah State University, 4100 Old Main Hill, Logan, UT, USA 5. Atmospheric and Space Technology Research Associates, LLC, 5777 Central Ave., Ste. 221, Boulder, CO, USA 6. Embry-Riddle Aeronautical University, 600 S. Clyde Morris Blvd., Daytona Beach, FL, USA 7. Space Dynamics Laboratory, North Logan, UT, USA 8. L-3 Communications, 640 N 2200 W, Salt Lake City, UT, USA 9. NASA Wallops Flight Facility, Wallops Island, VA, USA 10. LJT and Associates, 9881 Broken Land Parkway, Suite 400, Columbia, MD, USA 11. TiNi Aerospace, 2505 Kerner Blvd., San Rafael, CA, USA 12. SRI International, 333 Ravenswood Ave., Menlo Park, CA, USA |
| Abstract: | Funded by the NSF CubeSat and NASA ELaNa programs, the Dynamic Ionosphere CubeSat Experiment (DICE) mission consists of two 1.5U CubeSats which were launched into an eccentric low Earth orbit on October 28, 2011. Each identical spacecraft carries two Langmuir probes to measure ionospheric in-situ plasma densities, electric field probes to measure in-situ DC and AC electric fields, and a science grade magnetometer to measure in-situ DC and AC magnetic fields. Given the tight integration of these multiple sensors with the CubeSat platforms, each of the DICE spacecraft is effectively a “sensor-sat” capable of comprehensive ionospheric diagnostics. The use of two identical sensor-sats at slightly different orbiting velocities in nearly identical orbits permits the de-convolution of spatial and temporal ambiguities in the observations of the ionosphere from a moving platform. In addition to demonstrating nanosat-based constellation science, the DICE mission is advancing a number of groundbreaking CubeSat technologies including miniaturized mechanisms and high-speed downlink communications. |
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