NASA NTRS · 19710026702
Optimal N-burn multiorbit injection
Abstract
Procedure for computing gravity losses over n-burn multiorbit escape trajectories of specified final energy and prediction of optimal burn schedules for nuclear rocket escape maneuvers
Keep this discovery
Explore connections, maps & timelines
Singleton, R. L., Jr.. 1971-09-01. Optimal N-burn multiorbit injection. https://ntrs.nasa.gov/citations/19710026702
Cite the original work for its findings. Save a collection to share your selection of sources.