21![Maine Space Grant Consortium Maine Aerospace Workforce Development Program Student Research Experiences at NASA Field Centers Summer 2004 Maine Space Grant Consortium Maine Aerospace Workforce Development Program Student Research Experiences at NASA Field Centers Summer 2004](https://www.pdfsearch.io/img/48cf5aa5cc884faa919c8871fe57a6fb.jpg) | Add to Reading ListSource URL: www.msgc.orgLanguage: English - Date: 2013-11-19 18:44:00
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22![Efficient and high-performance propulsion system designed for use with xenon and iodine propellants. Busek’s BHT-8000 is a 8kW (nominal) Hall Effect thruster with state-of-the-art center mounted cathode and performance Efficient and high-performance propulsion system designed for use with xenon and iodine propellants. Busek’s BHT-8000 is a 8kW (nominal) Hall Effect thruster with state-of-the-art center mounted cathode and performance](https://www.pdfsearch.io/img/17369bcb5ce12c7927c50085e439ba91.jpg) | Add to Reading ListSource URL: www.busek.comLanguage: English - Date: 2016-07-28 14:45:39
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23![High performance and mature propulsion system with flight heritage, and the first US Hall effect thruster in space. The BHT-200 is a high performance and mature propulsion system with flight heritage aboard the Air Force High performance and mature propulsion system with flight heritage, and the first US Hall effect thruster in space. The BHT-200 is a high performance and mature propulsion system with flight heritage aboard the Air Force](https://www.pdfsearch.io/img/f57396527bdfec98f422e7c999ce38b7.jpg) | Add to Reading ListSource URL: www.busek.comLanguage: English - Date: 2016-07-28 14:45:38
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24![Efficient and high-performance propulsion system designed for use with xenon and iodine propellants. Busek’s BHT-1500 is a 2kW-class Hall Effect thruster with innovative center-mounted cathode. The center-mounted Efficient and high-performance propulsion system designed for use with xenon and iodine propellants. Busek’s BHT-1500 is a 2kW-class Hall Effect thruster with innovative center-mounted cathode. The center-mounted](https://www.pdfsearch.io/img/2204ffca9ca0a0545a688eb3e14a78c5.jpg) | Add to Reading ListSource URL: www.busek.comLanguage: English - Date: 2016-07-28 14:45:39
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25![Yes, This IS Rocket Science! Part 2 Does the shape of the nosecone affect the flight? Do the shape of the fins affect the flight? How about the length of the fuselage? Let’s see if we can figure that out! Yes, This IS Rocket Science! Part 2 Does the shape of the nosecone affect the flight? Do the shape of the fins affect the flight? How about the length of the fuselage? Let’s see if we can figure that out!](https://www.pdfsearch.io/img/987afb6e508347018374079fb40234a5.jpg) | Add to Reading ListSource URL: www.coopext.colostate.eduLanguage: English - Date: 2013-03-26 15:54:38
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26![Busek electrospray thrusters launch aboard ESA’s LISA Pathfinder on December 03, 2015. Satellite propulsion firm Busek Co. Inc. confirmed the launch of the world’s first flight-qualified electrospray thrusters on LIS Busek electrospray thrusters launch aboard ESA’s LISA Pathfinder on December 03, 2015. Satellite propulsion firm Busek Co. Inc. confirmed the launch of the world’s first flight-qualified electrospray thrusters on LIS](https://www.pdfsearch.io/img/2824f0949013030c0b27a101dc945511.jpg) | Add to Reading ListSource URL: www.busek.comLanguage: English - Date: 2016-07-28 14:45:40
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27![High-performance and long life propulsion system designed for use with xenon and iodine propellants. The BHT-600 is a mature propulsion system featuring high performance and compatibility with flight proven heritage comp High-performance and long life propulsion system designed for use with xenon and iodine propellants. The BHT-600 is a mature propulsion system featuring high performance and compatibility with flight proven heritage comp](https://www.pdfsearch.io/img/bdd3c40e99039d3297bc37a936d86fa9.jpg) | Add to Reading ListSource URL: www.busek.comLanguage: English - Date: 2016-07-28 14:45:38
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28![Dory: Design and Implementation of an Integrated, Autonomous Underwater Vehicle E. Fouad, T. Okamoto, F. Zhou, J. Orenstein, K. Agarwal, T. Pailevanian, J. Larson California Institute of Tec Dory: Design and Implementation of an Integrated, Autonomous Underwater Vehicle E. Fouad, T. Okamoto, F. Zhou, J. Orenstein, K. Agarwal, T. Pailevanian, J. Larson California Institute of Tec](https://www.pdfsearch.io/img/779117d102e0c7fdc7d8838331d2ec00.jpg) | Add to Reading ListSource URL: crt.caltech.eduLanguage: English - Date: 2016-06-27 15:04:25
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29![COMETWATER THRUSTER DSI Comet-1 CubeSat and Microsatellite Water Thrusters The Comet-1™ line of thrusters are simple, launch-safe, and cost-effective electrothermal propulsion systems that use water as a propel COMETWATER THRUSTER DSI Comet-1 CubeSat and Microsatellite Water Thrusters The Comet-1™ line of thrusters are simple, launch-safe, and cost-effective electrothermal propulsion systems that use water as a propel](https://www.pdfsearch.io/img/5360e337c3733cfaafc93c141764e0ee.jpg) | Add to Reading ListSource URL: deepspaceindustries.comLanguage: English - Date: 2016-08-04 20:05:01
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30![COMET-1 WATER THRUSTER The DSI Comet-1 CubeSat Electrothermal Water Thruster Comet-1 is a low-power, low-profile, high total impulse electrothermal micropropulsion system that uses water as propellant. Comet-1 is CubeSa COMET-1 WATER THRUSTER The DSI Comet-1 CubeSat Electrothermal Water Thruster Comet-1 is a low-power, low-profile, high total impulse electrothermal micropropulsion system that uses water as propellant. Comet-1 is CubeSa](https://www.pdfsearch.io/img/3ae1775442897ee996c31d3a72b5bf53.jpg) | Add to Reading ListSource URL: deepspaceindustries.comLanguage: English - Date: 2016-04-26 15:45:35
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