Optimal Trajectories for a Spacecraft Propelled by an E-Sail with Piecewise Inertially-fixed Attitude

Optimal Trajectories for a Spacecraft Propelled by an E-Sail with Piecewise Inertially-fixed Attitude

Item #:: 078371-0164
UPC:

Our Price: $30.00

Details

DOI: https://doi.org/10.52202/078371-0164
Author(s): Lorenzo Niccolai
Pages: 1483-1493 (11 pages)
Format: PDF Paper Download
Conference: IAF Space Propulsion Symposium
Date/Location: Held 14-18 October 2024, Milan, Italy.
Publisher: International Astronautical Federation (IAF)

Description

Members/Attendees

Tab 4

Details
Description
Members/Attendees
Tab 4

DOI: https://doi.org/10.52202/078371-0164
Author(s): Lorenzo Niccolai
Pages: 1483-1493 (11 pages)
Format: PDF Paper Download
Conference: IAF Space Propulsion Symposium
Date/Location: Held 14-18 October 2024, Milan, Italy.
Publisher: International Astronautical Federation (IAF)