Accession Number:

AD0603617

Title:

DESIGN OF A CONSTANT ATTITUDE TARGET FOR RENDEZVOUS WITH REMOTE MANEUVERING UNIT.

Descriptive Note:

Master's thesis,

Corporate Author:

AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1964-08-01

Pagination or Media Count:

159.0

Abstract:

A target satellite is designed to provide a test of the Remote Maneuvering Units rendezvous, television and radar capabilities and meet certain requirements imposed by NASA. A Fortran program is developed to calculate target trajectories based on perturbation theory and an atmospheric model which considers oblateness, solar heating and rotation.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE