Official name MARINER 5 (VENUS)
Alternative name Mariner 5
Cospar ID 1967-060A
Norad ID 2845
Launch date 1967-06-14
Launch site AFETR
Launch vehicle Atlas-SLV3 Agena-D
Country/Organization USA
Type application Venus flyby
Operator NASA
RCS size UNKNOWN
Decay date ON ORBIT
Shape Oct Cyl + 4 Pan
Mass (kg) 245
Diameter (m) 1.3
Height (m) 2.9
Span (m^2) 5.5
Contractors Jet Propulsion Laboratory (JPL)
Propulsion ?
Power 4 deployable fixed solar arrays, batteries

The Mariner 5 spacecraft was the fifth in a series of spacecraft used for planetary exploration in the flyby mode. Mariner 5 was a refurbished backup spacecraft for the Mariner 4 mission and was converted from a Mars mission to a Venus mission. 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. The spacecraft passed 4,000 km from Venus on 19 October 1967. 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. 

Satellite COSPAR Date LS Launch Vehicle Remarks
MARINER 5 (VENUS) 1967-060A 1967-06-14 AFETR Atlas-SLV3 Agena-D