K. I. Duck, William C. Isley
Abstract
Minimal electric propulsion systems for interplanetary spacecraft, discussing payload, reduced trip time and low thrust systems for Jupiter flyby
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Minimal electric propulsion systems for interplanetary spacecraft, discussing payload, reduced trip time and low thrust systems for Jupiter flyby
Key concepts: Electrically powered spacecraft propulsion, Interplanetary spaceflight, Spacecraft, Aerospace engineering, Propulsion, Ion thruster, Astrobiology, Spacecraft propulsion