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Analytic short period lunar and solar perturbations of artificial satellites
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Fisher, D. |
| Copyright Year | 1972 |
| Description | A short period luni-solar theory was generalized for application to arbitrary obliquity of the ecliptic and inclination of the moon's orbit to the ecliptic. Analytic first order lunar perturbations to the elements were derived. The theory is illustrated by an application to the communication satellite Intelsat 3F3. |
| File Size | 1001298 |
| Page Count | 33 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720016238 |
| Archival Resource Key | ark:/13960/t2f81437w |
| Language | English |
| Publisher Date | 1972-03-01 |
| Access Restriction | Open |
| Subject Keyword | Space Sciences Ecliptic Perturbation Orbital Elements Sun Lunar Effects Intelsat Satellites Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |