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Henry, M. D.

Publications and source records attributed to Henry, M. D..

The ion propulsion system for Dawn

The Dawn Project's mission is to rendezvous and map the two heaviest main belt asteroids Vesta and Ceres. The Ion Propulsion System (IPS) for Dawn will be used for the heliocentric transfer from the Earth to Vesta, orbit capture at Vesta, transfer to a low Vesta orbit, departure and escape from Vesta, the heliocentric transfer from Vesta to Ceres, orbit capture at Ceres, and transfer to a low Ceres orbit.

ion propulsion asteroids spacecraft NSTAR

DS1 ion propulsion emissions characterization

This paper describes the different electro static and electro magnetic emissions of the ion engine for each of the the thrust levels the engine has operated in space and in the test chamber.

Deep Space 1