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Zenit-A
RD-170 Credit: © Mark Wade |
LOx/Kerosene propellant rocket stage. Modification of same stage used as strap-on for Energia launch vehicle.
AKA: Zenit-1. Status: Active. Thrust: 8,181.13 kN (1,839,191 lbf). Gross mass: 354,300 kg (781,000 lb). Unfuelled mass: 28,600 kg (63,000 lb). Specific impulse: 337 s. Specific impulse sea level: 311 s. Burn time: 150 s. Height: 32.90 m (107.90 ft). Diameter: 3.90 m (12.70 ft). Span: 3.90 m (12.70 ft).
Cost $ : 30.000 million.
Subtopics
| Energia Strapon LOx/Kerosene propellant rocket stage. Essentially identical to Zenit stage 1. |
Country:
Ukraine.
Engines:
RD-171.
Launch Vehicles:
Zenit-2,
Zenit-2 11K77.05,
Zenit-3SL,
Zenit-2M,
Zenit-3SLB.
Propellants:
Lox/Kerosene.
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