NASA NTRS · 19760020214
Reference mission 3B ascent trajectory. Mission planning, mission analysis and software formulation
Abstract
Mission 3B is designed as a payload retrieval mission with both shuttle launch and orbiter landing to take place at the western test range. The mission is designed for direct rendezvous with a passive satellite in a 100 NMI circular orbit with an inclination of 104 degrees. The ascent portion of mission 3B is described as well as the trajectory simulation.
Keep this discovery
Explore connections, maps & timelines
Kuhn, A. E.. 1975-02-11. Reference mission 3B ascent trajectory. Mission planning, mission analysis and software formulation. https://ntrs.nasa.gov/citations/19760020214
Cite the original work for its findings. Save a collection to share your selection of sources.