NASA NTRS · 19760026147
Return-to-launch-site trajectory shaping
Abstract
The results are presented of a study to show the effect on flyback trajectories of constant inertial attitude during the fuel dissipation phase of a return-to-launch-site abort. It is shown that the value of the constant inertial attitude can be chosen to shape the flyback trajectory.
Keep this discovery
Explore connections, maps & timelines
Bown, R. L.. 1975-10-17. Return-to-launch-site trajectory shaping. https://ntrs.nasa.gov/citations/19760026147
Cite the original work for its findings. Save a collection to share your selection of sources.