|Name||D3 CubeSat (Drag De-Orbit Device CubeSat)|
|Units or mass||2U|
|Status||Operational? (Press release on 2022-09-14 but no reports with data on SatNOGS as of 2022-12-20)|
|Deployer||NRCSD (NanoRacks CubeSat Deployer) [Quad-M]|
|Launcher||Falcon 9 (ELaNa 45) (CRS-25)|
|Deployment||Deployed from ISS on 2022-09-06|
|Organisation||University of Florida|
|Entity||Academic / Education|
Demonstrate a simple, reliable, low-cost, non-propulsive system for deliberate deorbit.
Develop and demonstrate a simple, reliable, low-cost, non-propulsive system for deliberate deorbit of small spacecraft, including CubeSats. In order to achieve this goal, the project’s focus is on developing a proof-of-concept design that will control the orbital decay, up to the atmospheric ballistic entry point, of CubeSat form factors up to 12U.
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