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Mariner 10

Mariner 10
Mariner 10 transparent.png
The Mariner 10 spacecraft
Mission type Planetary exploration
Operator NASA / JPL
COSPAR ID 1973-085A
SATCAT № 6919
Mission duration 1 year, 4 months, 12 days
Spacecraft properties
Manufacturer Jet Propulsion Laboratory
Launch mass 502.9 kilograms (1,109 lb)
Power 820 watts (at Venus encounter)
Start of mission
Launch date November 3, 1973, 05:45:00 (1973-11-03UTC05:45Z) UTC
Rocket Atlas SLV-3D Centaur-D1A
Launch site Cape Canaveral LC-36B
End of mission
Disposal Decommissioned
Deactivated March 24, 1975 (1975-03-25)
Flyby of Venus
Closest approach February 5, 1974
Distance 5,768 kilometers (3,584 mi)
Flyby of Mercury
Closest approach March 29, 1974
Distance 704 kilometers (437 mi)
Flyby of Mercury
Closest approach September 21, 1974
Distance 48,069 kilometers (29,869 mi)
Flyby of Mercury
Closest approach March 16, 1975
Distance 327 kilometers (203 mi)
← Mariner 9

Mariner 10 was an American robotic space probe launched by NASA on November 3, 1973, to fly by the planets Mercury and Venus.

Mariner 10 was launched approximately two years after Mariner 9 and was the last spacecraft in the Mariner program. (Mariner 11 and 12 were allocated to the Voyager program and redesignated Voyager 1 and Voyager 2.)

The mission objectives were to measure Mercury's environment, atmosphere, surface, and body characteristics and to make similar investigations of Venus. Secondary objectives were to perform experiments in the interplanetary medium and to obtain experience with a dual-planet gravity assist mission. Mariner 10's science team was led by Bruce C. Murray at the Jet Propulsion Laboratory.

Mariner 10 was the first spacecraft to make use of an interplanetary gravitational slingshot maneuver, using Venus to bend its flight path and bring its perihelion down to the level of Mercury's orbit. This maneuver, inspired by the orbital mechanics calculations of the Italian scientist Giuseppe Colombo, put the spacecraft into an orbit that repeatedly brought it back to Mercury. Mariner 10 used the solar radiation pressure on its solar panels and its high-gain antenna as a means of attitude control during flight, the first spacecraft to use active solar pressure control.


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