Zenit 2
| Status | Retired |
|---|---|
| Rocket family | Zenit |
| Country | Soviet Union |
| Manufacturer | Yuzhmash |
| Number of orbital launches | 37 |
| First launch | 1985-04-13 |
| Last launch | 2004-06-10 |
Launches by year:
Latest launches:
| Launch date | Launch site | Rocket / Variant | Payload | Notes | Status |
|---|---|---|---|---|---|
| 2004-06-10 | Baikonur | Zenit 2 | Tselina-2 22 | success | |
| 2001-12-10 | Baikonur | Zenit 2 | Meteor 3M-N1/microsats | success | |
| 2000-09-25 | Baikonur | Zenit 2 | Orlets-2 2 | success | |
| 2000-02-03 | Baikonur | Zenit 2 | Kosmos 2369 (Tselina-2 18) | success | |
| 1999-07-17 | Baikonur | Zenit 2 | Okean-O 1 | success | |
| 1998-09-09 | Baikonur | Zenit 2 | Globalstar 12 sats | failure | |
Computer error caused a very premature engine shutdown during second stage burn. | |||||
| 1998-07-28 | Baikonur | Zenit 2 | Tselina-2 20 | success | |
| 1998-07-10 | Baikonur | Zenit 2 | Resurs-1 2/microsats | success | |
| 1997-09-04 | Baikonur | Zenit 2 | Tselina-2 18 | success | |
| 1997-05-20 | Baikonur | Zenit 2 | Tselina-2 #19 | failure | |
Strut in first stage engine failed at T+48 seconds. | |||||
| + 27 more... | |||||
Variants:
(This section is under construction)Zenit 2 Base variant
| First launch | 1985-04-13 |
|---|---|
| Stages | 2 |
| Mass | 460 t |
| Height | 57.4 m |
| Diameter | 3.9 m |
Payload capacity:
| LEO | 13740 kg to 200 km / 51.6 deg |
|---|