Performance of the NSTAR ion propulsion system on the Deep Space One mission
This paper provides an overview of the system and presents the flight validation data from the first 7600 hours of ion propulsion system operation in interplanetary space.
Engineering topics
Publications and source records attributed to Kakuda, R..
This paper provides an overview of the system and presents the flight validation data from the first 7600 hours of ion propulsion system operation in interplanetary space.
Explore the source record for details and available documents.
This paper provides an overview of the system and presents the first flight validation data on an ion propulsion system in interplanetary space.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Deep Space 1 is the first interplanetary spacecraft to use an ion propulsion system for the primary delta-v maneuvers. The purpose of the mission is to validate a number of technologies, including ion propulsion and a high degree of spacecraft autonomy, on a flyby of an asteroid and two comets.
This paper shows that existing solar electric ion propulsion technology can deliver substantial payloads to important small bodies for an effective cost.