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ENERGIYA launch vehicle


ENERGIYA
US DoD: SL-17

* Developer:
NPO Energiya
* Payload:
- more than 100,000 kg to LEO
- 22,000 kg Geosynchronous Orbit
* Chronology:
- First Launch Date : 05/15/1987
- Last Launch Date : 11/15/1988
- Launches
    Total Number: 2
    Number of Failure: 0
- Success Rate : 100 %
* Launch Vehicle:
- Total Mass: 2,419,000 kg
- Empty Mass: about 300,000 kg
- Liftoff Thrust: 3,582,253 kgf
- Total Length: 58,76 m
- Core Diameter: 7,75 m

Energia

ENERGIYA

* Stage 2: (Energiya RCS Retro & Correction Stage)
- Engine: RD-58 11D58D
- Number of Engines: 1
- Total Thrust (vac): 8,661 kgf
- Specific Impulse: 352 sec
- Burn Time: 680 sec
- Control Engine Burn Time: 0 sec
- Gross Mass: 17,000 kg
- Empty Mass: 2,000 kg
- Propellants: Kerosene / LOX
- Length: 5.70 m
- Core Diameter: 3.70 m

Stage 1

* Stage 1: (Energiya Core)
- Engine: RD-01200 11D122 RO-200
- Number of Engines: 4
- Total Thrust (vac): 800,286 kgf
- Specific Impulse: 453 sec
- Burn Time: 480 sec
- Control Engine Burn Time: 354 sec
- Gross Mass: 905,000 kg
- Empty Mass: 85,000 kg
- Propellants: LH2 / LOX
- Length: 58.76 m
- Core Diameter: 7.80 m
* Stage 0:   (4 x Energiya Strapon)
- Engine: RD-170 11D251
- Number of Engines: 4 x 4
- Total Thrust (vac): 4 x 806,400 kgf
- Burn Time: 145 sec
- Specific Impulse: 337 sec
- Control Engine Burn Time: 309 sec
- Gross Mass: 4 x 355,000 kg
- Empty Mass: 4 x 35,000 kg
- Propellants: Kerosene / LOX
- Length: 36.46 m
- Core Diameter: 3.90 m
- max.Span: 4.20 m

Stage 2

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ENERGIYA launch vehicle    

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