Venera 14 |
Russia |
Spacecraft n°: |
Russia satellite n°: |
| Designation | 12938 / 81110A |
| Launch date | 04 Nov 1981 - 05:31 UT |
| Launch site | B, LC-200/39 |
| Launch vehicle | Proton-K/D-1 8K82K (#311-02/11S824M) |
| Mission | Venus lander |
| Satellite type | 4V-1M N° 761 |
| Heliocentric (Solar) orbit | |
| Perihelion / Aphelion | 0.71 x 0.99 A.U. |
| Eccentricity | 0.17 |
| Inclination | 2.3? deg |
| Period | 286 days |
| Prime contractor | Lavochkin? |
| Operator | |
| Platform | |
| Mass at launch | kg |
| Dry Mass | 2460? kg (empty) |
| Basic shape | Cylinder + 2 panels |
| Dimension | 2.7 long - 2.3 dia - 5.7 span |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime | Indefinite |
| Ref.: #1, #7, #206 - update: 13.07.08 | Home |