200W HALL THRUSTER SYSTEM, FALCONSAT-5 (LAUNCHED 2010, SUCCESS)   The Space Plasma Characterization Source was delivered to USAFA for the FalconSat-5 mission.  This integrated unit  consists of cold ammonia gas, 200-800W Hall Effect Thruster, high speed plasma probe, neutral source, propellant  management system, power processing unit (PPU), instrument electronics and digital control interface unit (DCIU).  The  SPCS was launched in December 2010.  The SPCS was designed, fabricated, tested and delivered 18 months ATP. CONTACT: Lawrence Byrne Program Manager larry@busek.com
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