Mariner Mission to VenusJet Propulsion Laboratory (U.S.)
Science
Mariner Mission to Venus
Jet Propulsion Laboratory (U.S.)
Project Mariner (U.S.)
Furthermore, Goldstone engineers estimate that, if Mariner II had
continued to function in all its systems and to point its directional
antenna at the Earth, useful telemetry data could have been obtained by
the DSIF stations out to about 150 to 200 million miles, and tracking
data could have been secured from as far as 300 to 400 million miles.
Construction of the DSIF net was begun in 1958. The Goldstone station
was ready for the Pioneer III mission in December of that year. In
March, 1959, Pioneer IV was successfully tracked beyond the Moon. Later
in 1959, Pioneer V was tracked out to over 3 million miles.
Goldstone participated in the 1960 Project Echo communication satellite
experiments and the entire net was used in the Ranger lunar missions of
1961-1962. The Goldstone station performed Venus radar experiments in
1961 and 1962 to determine the astronomical unit more precisely and to
study the rotation rate and surface characteristics of the planet.
Following the launch of Mariner II on August 27, 1962, the full DSIF net
provided 24-hour-per-day tracking coverage throughout the mission except
for a few days during the cruise phase. The net remained on the
full-coverage schedule through the period of Venus encounter on December
14.
THE GOLDSTONE COMPLEX
The tracking antennas clustered in a 7-mile radius near Goldstone Dry
Lake, California, are the central complex of the DSIF net. Three
tracking sites are included in the Goldstone Station: Pioneer Site (DSIF
2), Echo Site (DSIF 3), and Venus Site. The Venus Site is used for
advanced radar astronomy, communication research experiments, and radio
development; it took no direct part in the Mariner spacecraft tracking
operations, but was used for the Venus radar experiments.
Pioneer Site has an 85-foot-diameter parabolic reflector antenna and the
necessary radio tracking, receiving, and data recording equipment. The
antenna can be pointed to within better than 0.02 of a degree. The
antenna has one (hour-angle) axis parallel to the polar axis of the
Earth, and the other (declination) axis perpendicular to the polar axis
and parallel to the equatorial plane of the Earth. This “polar-mount”
feature permits tracking on only one axis without moving the other.
The antenna weighs about 240 tons but can be rotated easily at a maximum
rate of 1 degree per second. The minimum tracking rate or antenna swing
(0.250686486 degree per minute) is equal to the rotation rate of the
Earth. Two drive motors working simultaneously but at different speeds
provide an antibacklash safety factor. The antenna can operate safely in
high winds.
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