QB50 System Requirements Document
QB50 System Requirements Document
QB50 System Requirements Document
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2.3 Spacecraft Contamination<strong>QB50</strong>-SYS-2.3.1. The CubeSat shall withstand a total contamination of 3.1mg/m 2(TBC before CDR) at all phases of the launch vehicle groundoperation and in flight.2.4 Electromagnetic Compatibility (EMC)<strong>QB50</strong>-SYS-2.4.1. During prelaunch processing and launch, the spacecraft onboardequipment and ground support equipment (GSE) shall sustain theelectromagnetic fields of up to 10V/m (TBC) within 10 kHz to 40GHz.Issue 3 18 5 February 2013