Viking 2

USA


Spacecraft nº:

USA satellite nº:

Also called: Viking Orbiter 2

Launch data:

Designation  08199 / 75083A
Launch date  09 Sep 1975 - 18:39 UT
Launch site CC, LC-41
Launch vehicle  Titan-3E Centaur-D1T (#23E-3/TC-3)
Mission  Mars orbiter
Satellite type 
Heliocentric orbit
Perihelion / Aphelion  1.006 x 1.669 AU
Eccentricity 0.248
Inclination 2.92 deg
Period  565 days
Mars orbit on 1976 Aug 07.47:
Perihelion / Aphelion  1502 x 35728 km
Eccentricity 0.778
Inclination 55.6 deg
Period  1644.6 min
Mars orbit on 1976 Dec 20:
Perihelion / Aphelion  787 x 35463 km
Eccentricity 0.806
Inclination 80 deg
Period  1590 min
Mars orbit on 1977 Oct 23:
Perihelion / Aphelion  302 x 33176 km
Eccentricity 0.816
Inclination 80.3 deg
Period  1439 min


Spacecraft data:

Prime contractor  
Operator 
Platform  
Mass at launch  2325 kg (full)
Dry Mass  kg
Basic shape  Octagonal box + 4 vanes
Dimension  3.3 high - 1.8 wide - 1.5 deep
Solar array  
Stabilization  
DC power  
Design lifetime  44 years? - In Mars orbit

Viking lander model


Mission details:


On September 3, 1976, Viking 2 lands on Utopia Planitia on Mars. It would function for 1,316 days, finally shutting down on April 11, 1980.



Ref.: #1, #7(JR326), #117, #206, #307 - update: 13.07.08 Home