Approximate stability criteria for highly eccentric orbits about the earth.Stability analysis of highly eccentric satellite orbits about earth in lunar-solar gravitational disturbing field, deriving approximate criteria from planetary perturbation theory
Document ID
19680063316
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Renard, M. L.
Date Acquired
August 4, 2013
Publication Date
October 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AND INTERNATIONAL ASTRONAUTICAL FEDERATION.
Subject Category
Space Sciences
Report/Patent Number
IAF PAPER AD-83Report Number: IAF PAPER AD-83
Meeting Information
Meeting: CONGRESS OF THE INTERNATIONAL ASTRONAUTICAL FEDERATION