Abstract
The celestial bodies are considered as mass-points attracting each other according to Newton's law. Khilmi (1961) obtained some sufficient conditions for the occurrence of disintegration and escape in then-body system as time tends to infinity using his theory of continuous induction, inductiveness of inequalities and α-approach. Making an analytic approach, an improved version of Khilmi's result on escape and conditions to avoid disintegration is obtained.
Similar content being viewed by others
References
Chazy, J.: 1922,Ann. Sci. Ecole Norm. 39.
Corben, H. C. and Stehle, P.: 1960,Classical Mechanics, 2nd Edition, Wiley, New York.
Khilmi, G. F.: 1961,Qualitative Methods in the Many Body Problem, Gordon and Breach, New York.
Pollard, H.: 1970, ‘Disintegration and Escape’, in G. E. D. Giacaglia (ed.),Periodic Orbits, Stability and Resonances, D. Reidel Publishing Company, Dordrecht-Holland, pp. 53–55.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Patnaik, R.B. The problem of escape in then-body system. Celestial Mechanics 12, 383–390 (1975). https://doi.org/10.1007/BF01228570
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF01228570