Venera 2
From Wikipedia, the free encyclopedia
Venera 2 (Russian: Венера-2) (manufacturer's designation: 3MV-4) was a probe in the Soviet Venera program for the exploration of Venus.
- Launch Date/Time: 1965 November 12 at 05:02:00 UTC
- On-orbit Dry Mass: 963 kg
Venera 2 was launched from a Tyazheliy Sputnik (65-091B) towards the planet Venus and carried a TV system and scientific instruments. On February 27, 1966, the spacecraft passed Venus at a distance of 24,000 km and entered a heliocentric orbit. The spacecraft system had ceased to operate before the planet was reached and returned no data.
|
|
|
| Flybys |
|
|
|
| Orbiters |
|
|
| Descent probes |
|
|
| Landers |
|
|
| Balloon probes |
|
|
| Future missions |
|
|
| Proposed missions |
|
|
| See also |
|
|
- Bold italics indicates active missions
|
|
|
|
|
|
|
|
|
Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets.
|
|