Zenit-3

Zenit-3SLB
by Mr.Sirus Iton from Wikipedia

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:

b14643.de – Zenit-3

b14643.de – Zenit-3SL

Wikipedia – Zenit-3F

Wikipedia – Zenit-3SL

Wikipedia – Zenit-3SLB

Destination Orbite

Space Launch Report

Encyclopedia Astronautica – Zenit-3SL

Encyclopedia Astronautica – Zenit-3SLB

Russian Space Web

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