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Dynamic Ionosphere CubeSat Experiment

From Wikipedia, the free encyclopedia
Cubesats studying space weather

TheDynamic Ionosphere CubeSat Experiment (DICE) is a scientific mission consisting of twoMiniaturized SatellitesDICE-1 andDICE-2 flying in formation.[1] The satellites are an unusual 1.5U variant of theCubeSat design for microsatellites. Both satellites were launched fromVandenberg Air Force Base in October 2011 atop aDelta IIrocket. This was a multi-payload mission with four other CubeSats,AubieSat-1,M-Cubed,Explorer-1_Prime andRAX-2.[2]

The satellites are intended to map changes in the Earth'sPlasmasphere caused byGeomagnetic storms.[3]

On board control is provided by a Pumpkin FM430 flight control module containing aTexas Instruments MPS430microcontroller. Communications are provided by ahalf-duplexUHFmodem 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 DCLangmuir probes for detection ofions and a three-axismagnetometer for measuringmagnetic fields.[4]

References

[edit]
  1. ^Krebs, Gunter D."DICE 1, 2 (Yahtzee, Farkle)". Gunter's Space Page. RetrievedDecember 10, 2022.
  2. ^Graham, William (October 28, 2011)."Delta II successfully launches NPP satellite on behalf of NASA and NOAA". NASASpaceflight.com. RetrievedDecember 9, 2022.
  3. ^"Satellite Missions Catalogue: DICE (Dynamic Ionosphere CubeSat Experiment)". eoPortal.org. RetrievedDecember 9, 2022.
  4. ^Burr, Steven Reed (2013).The Design and Implementation of the Dynamic Ionosphere Cubesat Experiment (Dice) Science Instruments" (Report). RetrievedDecember 9, 2022.

External links

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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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