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Date: 2016-07-28 14:45:51Spacecraft propulsion Spaceflight Spacecraft Propulsion Busek Hall-effect thruster Ion thruster USA-221 Electrically powered spacecraft propulsion TacSat-2 Specific impulse Thruster | Busek’s low power Hall Effect Thrusters span between 100 and 1500 W Typical low power Isp range: 1100 to 2000 s Busek Co. has been developing next generation high performance electric propulsion systems. Our family ofAdd to Reading ListSource URL: www.busek.comDownload Document from Source WebsiteFile Size: 939,79 KBShare Document on Facebook |
Experience with Rule-Based Analysis of Spacecraft Logs? Klaus Havelund and Rajeev Joshi Jet Propulsion Laboratory California Institute of Technology California, USADocID: 1xUdS - View Document | |
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Resolving Spacecraft Earth-Flyby Anomalies with Measured Light Speed Anisotropy Reginald T. Cahill arXiv:0804.0039v3 [physics.gen-ph] 9 Apr 2008DocID: 1uFIe - View Document |