EARTH-TO-MOON TRAJECTORIES IN THE RESTRICTED THREE-BODY PROBLEM.

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Abstract:

Motion of a particle of negligible mass from the neighborhood of a gravitational center the earth of mass 1-mu to the neighborhood of a second center the moon of mass mu is studied within the framework of the restricted threebody problem by asymptotic methods for the case mu 1.

Author(s):
Lagerstrom, P. A. ; Kevorkian, J. K.
Author Organization(s):
DOUGLAS AIRCRAFT CO INC SANTA MONICA CALIF
Descriptive Note:
Engineering paper,
Annotation:
Earth-to-moon trajectories in the restricted three-body problem.
Pagination:
0060

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
EP1646, AFOSR-J886
Contract/Grant Number(s):
AF AFOSR62 256
Monitor Series:
J886
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*N BODY PROBLEM, PERTURBATION THEORY, TRAJECTORIES, ORBITS, EARTH(PLANET), MOON, PARTICLES, ENERGY, TIME, GRAVITY, VELOCITY, MOMENTUM, BOUNDARY LAYER, INTEGRALS, DIFFERENTIAL EQUATIONS, POLYNOMIALS, FUNCTIONS(MATHEMATICS), CELESTIAL MECHANICS, SPACE FLIGHT
Report Date:
1963 May 22