Dynamic Ionosphere CubeSat Experiment
The Dynamic Ionosphere CubeSat Experiment (DICE) is a scientific mission consisting of two Miniaturized Satellites DICE-1 and DICE-2 flying in formation.[1] The satellites are an unusual 1.5U variant of the CubeSat design for microsatellites. Both satellites were launched from Vandenberg Air Force Base in October 2011 atop a Delta II rocket. This was a multi-payload mission with four other CubeSats, AubieSat-1, M-Cubed, Explorer-1_Prime and RAX-2.[2]
The satellites are intended to map changes in the Earth's Plasmasphere caused by Geomagnetic storms.[3]
On board control is provided by a Pumpkin FM430 flight control module containing a Texas Instruments MPS430 microcontroller. Communications are provided by a half-duplex UHF modem with a 1.5 Mbit/s downlink (465 MHz) and 19.2 kbit/s uplink (450 MHz). The satellites carry four Electric Field Probe sensors on telescopic booms, two DC Langmuir probes for detection of ions and a three-axis magnetometer for measuring magnetic fields.[4]
References
- ^ Krebs, Gunter D. "DICE 1, 2 (Yahtzee, Farkle)". Gunter's Space Page. Retrieved December 10, 2022.
- ^ Graham, William (October 28, 2011). "Delta II successfully launches NPP satellite on behalf of NASA and NOAA". NASASpaceflight.com. Retrieved December 9, 2022.
- ^ "Satellite Missions Catalogue: DICE (Dynamic Ionosphere CubeSat Experiment)". eoPortal.org. Retrieved December 9, 2022.
- ^ Burr, Steven Reed (2013). The Design and Implementation of the Dynamic Ionosphere Cubesat Experiment (Dice) Science Instruments" (Report). Retrieved December 9, 2022.
External links
- Space Dynamics Laboratory Small Satellites
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- Kosmos 2470
- USA-225
- Johannes Kepler ATV
- STS-133 (Leonardo)
- Kosmos 2471
- Glory, Explorer-1 [Prime], KySat-1, Hermes
- USA-226
- USA-227
- Shijian XI-03
- STS-135 (Raffaello, PSSC-2)
- Tianlian I-02
- Globalstar M083, Globalstar M088, Globalstar M091, Globalstar M085, Globalstar M081, Globalstar M089
- GSAT-12
- SES-3, KazSat-2
- USA-232
- Spektr-R
- Compass-IGSO4
- Shijian XI-02
- Juno
- Astra 1N, BSAT-3c/JCSAT-110R
- Paksat-1R
- Hai Yang 2A
- Sich 2, NigeriaSat-2, NigeriaSat-X, RASAT, EduSAT, AprizeSat-5, AprizeSat-6, BPA-2
- Ekspress-AM4
- Shijian XI-04
- Progress M-12M
- GRAIL-A , GRAIL-B
- Zhongxing-1A
- Kosmos 2473
- Arabsat 5C, SES-2
- IGS Optical 4
- Atlantic Bird 7
- TacSat-4
- Tiangong-1
- QuetzSat 1
- Kosmos 2474 / GLONASS-M 742
- Intelsat 18
- Eutelsat 16A
- Megha-Tropiques, SRMSAT, VesselSat-1, Jugnu
- ViaSat-1
- Galileo-IOV FM1 , Galileo-IOV FM2
- NPP, AubieSat-1, DICE-1, DICE-2, M-Cubed, RAX-2
- Progress M-13M
- Shenzhou 8
- Kosmos 2475 , Kosmos 2476 , Kosmos 2477
- Fobos-Grunt , Yinghuo-1
- Yaogan 12 , Tian Xun-1
- Soyuz TMA-22
- Shiyan Weixing 4 , Chuang Xin 1C
- AsiaSat 7
- Mars Science Laboratory (Curiosity)
- Kosmos 2478
- Yaogan 13
- Compass-IGSO5
- Amos-5, Luch 5A
- IGS Radar 3
- Pléiades-HR 1A, SSOT, ELISA 1, ELISA 2, ELISA 3, ELISA 4
- NigComSat-1R
- Soyuz TMA-03M
- Ziyuan-1C
- Meridian 5
- Globalstar M080, Globalstar M082, Globalstar M084, Globalstar M086, Globalstar M090, Globalstar M092
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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