NASA NTRS · 19710000374
New procedure for determining minimum time orbit transfers
Abstract
Computer program includes time minimizing function required for propellant constrained minimum time impulsive transfer between coplanar circular orbits or unrestricted orbits. Basic formulation is extended to include inclined circular or inclined elliptic orbits.
Keep this discovery
Explore connections, maps & timelines
Davis, D. A.. 1971-10-01. New procedure for determining minimum time orbit transfers. https://ntrs.nasa.gov/citations/19710000374
Cite the original work for its findings. Save a collection to share your selection of sources.