NASA NTRS · 19690043213
Mission analysis model requirements for electric propulsion.
Abstract
Spacecraft electric propulsion parameters and launching vehicle characteristics in low thrust mission simulation, discussing spacecraft path
Keep this discovery
Explore connections, maps & timelines
Barber, T. A.. 1969-01-01. Mission analysis model requirements for electric propulsion.. https://ntrs.nasa.gov/citations/19690043213
Cite the original work for its findings. Save a collection to share your selection of sources.