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Smallsat designers now have the opportunity to choose from a variety of commercial-off-the-shelf (COTS) propulsion options, which are broadly categorized into chemical, cold gas, and electric propulsion systems. This manuscript provides an overview and comparison of the propulsion systems that are available for smallsat missions in terms of the wet mass required across increasing orbit lifetimes and their delivered mass capability for a given delta-v impulse.

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This page is a summary of: Survey and Performance Evaluation of Small-Satellite Propulsion Technologies, Journal of Spacecraft and Rockets, October 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34774.
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