Zenit-3

Country of Origin: Ukraine
Manufacturer: Yuzhnoye
Height: 59.6 m
Diameter: 3.9 m
Payload to LEO: (3.75 to 6.16 tons to GTO)
Total Mass: 471 tons
Launch Sites: Baikonur, Ocean Odyseey
First Flight: March 28, 1999
Last Flight: Active
Total Launches: 45
Successful Launches: 41
Zenit-3F
Stage | Diameter | Fuel | Engine | Time | Thrust (Vac.) | ISP (SL / Vac.) | Mass / Empty Mass |
---|---|---|---|---|---|---|---|
1 | 3.9 m | RP-1 / LOX | RD-171 | 140-150 s | 7908 kN | ? / 337.2 s | 354.35 tons / 27.56 tons |
2 | 3.9 m | RP-1 / LOX | RD-120 + RD-8 verniers | 360-370 s | 912 kN + 79.4 kN | ? / 349 s | 90.79 tons / 8.3 tons |
3 (Fregat-SB) | UDMH / N2O4 | S5.92 | 1635 s | 20.01 kN | ? / 327 s | 11.56 tons / 1.41 tons |
Zenit-3SL
Stage | Diameter | Fuel | Engine | Time | Thrust (Vac.) | ISP (SL / Vac.) | Mass / Empty Mass |
---|---|---|---|---|---|---|---|
1 | 3.9 m | RP-1 / LOX | RD-171 | 140-150 s | 7908 kN | ? / 337.2 s | 354.35 tons / 27.56 tons |
2 | 3.9 m | RP-1 / LOX | RD-120 + RD-8 verniers | 360-370 s | 912 kN + 79.4 kN | ? / 349 s | 90.79 tons / 8.3 tons |
3 (Block DM-SL) | 3.7 m | RP-1 / LOX | RD-58M | 650 s | 84.9 kN | ? / 352 s | 17.36 tons / 2.14 tons |
Zenit-3SLB
Stage | Diameter | Fuel | Engine | Time | Thrust (Vac.) | ISP (SL / Vac.) | Mass / Empty Mass |
---|---|---|---|---|---|---|---|
1 | 3.9 m | RP-1 / LOX | RD-171 | 140-150 s | 7908 kN | ? / 337.2 s | 354.35 tons / 27.56 tons |
2 | 3.9 m | RP-1 / LOX | RD-120 + RD-8 verniers | 360-370 s | 912 kN + 79.4 kN | ? / 349 s | 90.79 tons / 8.3 tons |
3 (Block DM-SL) | 3.7 m | RP-1 / LOX | RD-58M | 650 s | 84.9 kN | ? / 352 s | 17.36 tons / 2.14 tons |
Links:
Encyclopedia Astronautica – Zenit-3SL