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Conceptual Design for JPL’s Micro Surveyor Planetary Spacecraft
Conceptual Design for JPL’s Micro Surveyor Planetary Spacecraft This concept spacecraft would stand just 0.9 m high. The design is sized to fit within the space allocated for secondary payloads adapter ring (ESPA) on the launch of larger spacecraft (insert figure in the upper right). Propulsion would be provided by an electric propulsion system (EP). JPL