Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19670053712

Restricted three-body problem in the post- Newtonian approximation.

View original source ↗Export metadata ↓

Abstract

Restricted three-body problem in post-Newtonian approximation, obtaining equations of motion

Explore related subjects

THREE-BODY PROBLEM JACOBI INTEGRAL MOTION EQUATION

Keep this discovery

Explore connections, maps & timelines

Krefetz, E.. 1967-05-01. Restricted three-body problem in the post- Newtonian approximation.. https://ntrs.nasa.gov/citations/19670053712

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

NASA NTRS1967

A new Lie series method for the numerical integration of ordinary differential equations, with an application to the restricted problem of three bodies

New Lie series method for numerical integration of ordinary differential equations, and restricted three-body problem application

THREE-BODY PROBLEM↗

NASA NTRS1967

Systems analysis

Selenodesy experiment, data compression, Mars and Venus mass data, Earth-Moon mass ratio, orbits for three-body problem, and unbraked impact time for lunar landing mission - systems analyses

THREE-BODY PROBLEM↗

NASA NTRS1967

Stability studies of periodic solutions Final report

Stability of periodic orbits of restricted three- body problem

THREE-BODY PROBLEM↗