Session 4: Small NEA Mission Design Challenges Key Technology Requirements Technologies (Drivers, Uncertainties, and Gaps) John Dankanich NASA Marshall Space Flight Center July 9, 2013 - Variable Specific Impulse Magnetoplasma Rocket - Document - PDFSEARCH.IO

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	Session 4: Small NEA Mission Design Challenges Key Technology Requirements / Technologies (Drivers, Uncertainties, and Gaps) John Dankanich NASA Marshall Space Flight Center July 9, 2013 Add to Reading List Document Date: 2014-07-30 15:45:29 Open Document File Size: 1,44 MB Share Result on Facebook Company TA07 Human Exploration Destination Systems / Extravehicular Activity Systems / Autonomous Systems / Air Force Transformational Satellite Communication Systems / / Facility Hall Thruster Development Occurred / / IndustryTerm mobility technology / technology gaps / thruster technology / technology/system development / / Organization AFRL / National Aeronautics and Space Administration / Power Processing Unit / Nuclear Regulatory Commission / Asteroid Retrieval Mission / Shorter mission / Space Technology Mission Directorate / / Person Marshall Space / John Dankanich / / Position Xenon Flow Controller / / Product L-3 ETI / / Technology SOA / ISP / 3.2 Surface mobility technology / Hall thruster technology / / SocialTag Space technology Hall effect thruster Ion thruster Asteroid-impact avoidance Specific impulse Aerojet Electrostatic ion thruster Variable Specific Impulse Magnetoplasma Rocket Spacecraft propulsion Aerospace engineering

Session 4: Small NEA Mission Design Challenges Key Technology Requirements / Technologies (Drivers, Uncertainties, and Gaps) John Dankanich NASA Marshall Space Flight Center July 9, 2013Add to Reading List