The Mariner Mars 1971 (MM '71) orbiter spacecraft, launched toward Mars in the spring of 1971, was designed to offer the first opportunity for sustained observations in the near vicinity of another planet of our solar system. The MM '71 spacecraft, like its predecessors, is fully attitude stabilized about three axes, using the sun and Canopus as references, an orientation which allows use of photovoltaic solar panels for primary power and permits two-way communication to the earth through a high-gain directional antenna. Midcourse and orbit insertion maneuvers use the sun-Canopus orientation as a reference direction for initiating commanded turns. Scientific instruments employed during Mars orbital operations are mounted on a two-degree-of-freedom platform controlled by commands from the central computer and sequencer. Science measurements to be obtained by the MM '71 spacecraft include television visual imaging, infrared radiometry, infrared spectroscopy, ultraviolet spectroscopy, S-band radio occultation, and celestial mechanics.
The Mariner Mars 1971 orbiter.
World Congress of the International Federation of Automatic Control ; 1972 ; Paris, France
1972-01-01
Miscellaneous
No indication
English
Mariner Mars 1971 orbiter study report
NTRS | 1968
Mariner MARS 1971 Orbiter Study Report
NTIS | 1968
NTRS | 1970
Mariner MARS 1969 Orbiter Study Final Report
NTIS | 1964