Accession Number : AD0657156
Title : PERFORMANCE OF THE SUPPORT SYSTEMS ABOARD THE DME-A SATELLITE, 29 NOV. 1965-FEB. 1967.
Descriptive Note : Technical memo.,
Corporate Author : JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Personal Author(s) : Maranto,S. J.
Report Date : APR 1967
Pagination or Media Count : 113
Abstract : The report describes the performance of the support systems aboard the DME-A satellite, i.e., the attitude control, attitude detection, telemetry, command, antenna, and power systems, all of which were developed, fabricated, and tested by the Applied Physics Laboratory of The Johns Hopkins University. The scientific results obtained from the experiments aboard the satellite are not discussed in this document. The Introduction and Spacecraft Design sections of this report are presented to familiarize the reader with the project implementations and the basic design of the DME-A satellite, respectively. The DME-A satellite continues to successfully fulfill its mission objectives and provide useful scientific data, even after exceeding by over four months the one-year useful operating lifetime for which it was designed. (Author)
Descriptors : (*SCIENTIFIC SATELLITES, PERFORMANCE(ENGINEERING)), DESIGN, ATTITUDE CONTROL SYSTEMS, ATTITUDE INDICATORS, TELEMETER SYSTEMS, COMMAND AND CONTROL SYSTEMS, SATELLITE ANTENNAS, SOLAR CELLS, POWER SUPPLIES, SPACECRAFT COMPONENTS
Subject Categories : Aircraft
Electric Power Production and Distribution
Command, Control and Communications Systems
Distribution Statement : APPROVED FOR PUBLIC RELEASE