The mission
The QARMAN mission was a 3U CubeSat for the In-Orbit Demonstration (IOD) of a new low-cost small re-entry vehicle capability.
Mission description
The QubeSat for Aerothermodynamic Research and Measurements on Ablation (QARMAN) was originally planned to be embarked as an IOD CubeSat on the launch of the QB50 constellation, however eventually launched to ISS and deployed into orbit from where its altitude decayed until re-entry. The demonstration included the use and flight testing of novel re-entry heatshield materials and an innovative aerodynamic drag passive attitude stabilisation system as well as the use of Iridium Inter-satellite Links during re-entry in order to transmit re-entry related telemetry before reaching the Earth surface.
Mission status
Παράθυρο πολυμέσων
Qarman CubeSat: falling into a fireball
Qarman CubeSat in Hertz test chamber
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