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Trajectory analysis of transfers between l4 and l5 and low lunar orbit
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1988 |
| Description | The flight characteristics and spacecraft performance during missions involving flight between the equilateral libration points and the Moon are discussed. The conclusions drawn will show that a minimum energy trajectory is the most efficient transfer technique for this type of flight. |
| File Size | 1347114 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890005773 |
| Archival Resource Key | ark:/13960/t03z35627 |
| Language | English |
| Publisher Date | 1988-10-30 |
| Access Restriction | Open |
| Subject Keyword | Astrodynamics Bouguer Law Spacecraft Performance Gravitational Effects Moon Spacecraft Trajectories Transfer Orbits Mission Planning Lunar Bases Libration Many Body Problem Earth Planet Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
