NASA NTRS · 20060039366
Performance Estimate of Large-Scale Ion Engines for SEI-Type Missions Using C(sub 60) Propellant
Abstract
Engine performance parameter, such as thrust, efficiency, specific mass, thruster input, power, thrust-to-power ratio and discharge current have been calculated with specific impulse the indupendent variablel.
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Mueller, Juergen. 1993-01-01. Performance Estimate of Large-Scale Ion Engines for SEI-Type Missions Using C(sub 60) Propellant. https://ntrs.nasa.gov/citations/20060039366
Cite the original work for its findings. Save a collection to share your selection of sources.