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ZENIT-URAGAN launch vehicle


ZENIT - URAGAN
US DoD: SL-?

* Developer:
NPO Yuzhnoye (Ukraine)
* Payload:
- 1.000 kg to 220 km Orbit
* Chronology:
- First Launch Date : 08/01/1987
- Last Launch Date : 08/28/1987
- Launches
    Total Number: 2
    Number of Failure: 0
- Success Rate : 100 %
* Launch Vehicle:
- Total Mass: 461.900 kg
- Liftoff Thrust: 769,880 kgf
- Length with Faring: 56.00 m
- Core Diameter: 3.90 m

Zenit-Uragan

ZENIT URAGAN

* Spacecraft: 1/3 scale model of URAGAN
- Total Mass:

1,400 kg

- Length over all: 4.50 m
- Wing Span: 3.00 m
- Fuselage Diameter: 0.70 m

zenurf.gif (4879 Byte)

* solid rocket motors block:
- Engine: ??
- Number of Engines: 12
- Total Thrust (vac): ?? kgf
- Propellants: ??
- Length: 1.74 m
- Core Diameter (conical): 2.44 m
* 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: 11.50 m
- Core Diameter: 3.90 m

Stage 2 without Payload

* 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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