LONG-TERM EVOLUTION OF MEDIUM-DISTANCE ORBITS.
Abstract
A method is developed for predicting the long-term development of orbits having moderate to large eccentricities (0.33 < e < 0.9) and semi major axes up to 10 Earth radii. For many orbits of this type the lifetime depends entirely on the interaction of the luni-solar perturbations with the effects of the Earth's gravitational potential. Lifetime estimates are given for 8 satellites. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1965
- Accession Number
- AD0482734
Entities
People
- Diana W. Scott
- G. E. Cook
Organizations
- Royal Aircraft Establishment