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Orbit mechanics about small asteroids
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Scheeres, D. J. |
| Copyright Year | 2007 |
| Description | Space missions to small solar system bodies must deal with multiple perturbations acting on the spacecraft. These include strong perturbations from the gravity field and solar tide, but for small bodies the most important perturbations may arise from solar radiation pressure (SRP) acting on the spacecraft. Previous research has generally investigated the effect of the gravity field, solar tide, and SRP acting on a spacecraft trajectory about an asteroid in isolation and has not considered their joint effect. In this paper a more general theoretical discussion of the joint effects of these forces is given. |
| File Size | 424972 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080012725 |
| Archival Resource Key | ark:/13960/t6p034x5z |
| Language | English |
| Publisher Date | 2007-09-24 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Space Missions Gravitational Effects Spacecraft Trajectories Asteroids Gravitational Fields Isolation Perturbation Solar Radiation Tides Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |