Mariner 5

USA



Launch data:


Designation 02845 / 67060A
Launch date 14 Jun 1967 - 06:01 UT
Launch site CC, LC12
Launch vehicle Atlas-SLV3 Agena-D (#5401/AA23)
Satellite typeMariner 67-2
Mission Venus flyby
Heliocentric orbit
Perihelion x Aphelion 0.579 x 0.735 A.U.
Eccentricity0.119
Inclination1.37°
Period 195 days


Specifications:

Prime contractor  
Operator  
Platform  
Mass at launch ~1106 kg
Dry Mass 246 kg
Dimension 2.90 long - 1.27 dia
Basic shape Octagonal cylinder
Solar array  
Stabilization  
Lifetime Indefinite

Descriptions:

Mariner 5 was a refurbished backup spacecraft for the Mariner 4 mission and was converted from a Mars mission to a Venus mission. Mariner 5 carried a complement of experiments to probe Venus's atmosphere with radio waves, scan its brightness in ultraviolet light, and sample the solar particles and magnetic field fluctuations above the planet. Spacecraft: The spacecraft was fully attitude stabilized, using the sun and Canopus as references. A central computer and sequencer subsystem supplied timing sequences and computing services for other spacecraft subsystems. Octagonal bus structure with four solar panels.3-axis stabilised using cold gas thrusters. S-Band communications via LGA and HGA. Thermal shield. Payload: The spacecraft instruments measured both interplanetary and Venusian magnetic fields, charged particles, and plasmas, as well as the radio refractivity and UV emissions of the Venusian atmosphere. The mission was termed a success.

Mission details:


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