R-26-1

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R-26-1

8K66
Credit: © Mark Wade

Nitric acid/UDMH propellant rocket stage. Orevo has sectioned hardware. TsNIIMash has 1:10 structural simulation model. All figures accurate except empty mass estimated. Source: Placard, TsNIIMash, Orevo.

AKA: 8K66. Status: Out of production. Thrust: 1,451.00 kN (326,197 lbf). Gross mass: 60,300 kg (132,900 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 310 s. Specific impulse sea level: 251 s. Burn time: 160 s. Diameter: 3.00 m (9.80 ft). Span: 15.00 m (49.00 ft).

Country: Ukraine. Engines: RD-224. Launch Vehicles: R-26. Propellants: Nitric acid/UDMH.

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