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ZENIT-3 launch vehicle


ZENIT-3

* Developer:
NPO Yuzhnoye (Ukraine)
* Payload:
- 13,740 kg to 200 km Orbit
-   5,180 kg to Geosynchronous transfer trajectory

Faring

* Chronology:
- First Launch Date : 1998
- Last Launch Date : in service
- Launches
    Total Number: 0
    Number of Failure: 0
- Success Rate :   %
* Launch Vehicle:
- Total Mass: 461,900 kg
- Liftoff Thrust: 769,880 kgf
- Length with Faring: 49.90 m
- Core Diameter: 3.90 m

Zenit - 3 sea launch

ZENIT 3 sea launch

* Block DM-SL:
- Engine: RD-58 11D58D
- Number of Engines: 1
- Total Thrust (vac): 7,240 kgf
- Specific Impulse: 361 sec
- Burn Time: 660 sec
- Gross Mass: 17,300 kg
- Empty Mass: 3,100 kg
- Propellants: Kerosene / LOX
- Length: 5.50 m
- Length Faring: 8.54 m
- Core Diameter: 3.74 m

Block DM-SL

* Stage 2:
- Engine: RD-120 11D123
- Number of Engines: 1
- Total Thrust (vac): 93,000 kgf
- Specific Impulse: 349+?? sec
- Burn Time: 315+?? sec
- Gross Mass: 90,400+?? kg
- Empty Mass: 8,400+?? kg
- Propellants: Kerosene / LOX
- Length: 15.90 m
- Core Diameter: 3.90 m

Stage 2

* Stage 1:
- Engine: RD-171 11D520
- Number of Engines: 4
- Total Thrust (vac): 834,243 kgf
- Specific Impulse: 337 sec
- Burn Time: 150 sec
- Gross Mass: 354,200 kg
- Empty Mass: 27,900 kg
- Propellants: Kerosene / LOX
- Length: 32.06 m
- Core Diameter: 3.90 m

Stage 1

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