An investigation of the invariant orbital elements of primary large bodies with parabolic and hyperbolic orbits.
The present work studies briefly the invariant elements (semimajor axis and the quasi-constant Jacobi integral) of the orbits of fragments of primary large bodies. Expressions are derived for the minima and maxima of these elements. Results can be used in testing the hypothesis of the common origin of the asteroids and comets.
Akademiia Nauk Azerbaidzhanskoi SSR Izvestiia Seriia Fiziko Tekhnicheskikh i Matematicheskikh Nauk
- Pub Date:
- Jacobi Integral;
- Orbital Elements;
- Planetary Evolution;
- Angular Velocity;
- Extremum Values;