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8K94 stage
Part of RT-20P
N2O4/UDMH propellant rocket stage. Unusual designation for the upper stage of another Yangel project - possibly reflecting that the design originally was a stand-alone IRBM? Empty mass estimated.

AKA: 8K94. Status: Retired 1969. Thrust: 147.00 kN (33,046 lbf). Gross mass: 9,800 kg (21,600 lb). Unfuelled mass: 900 kg (1,980 lb). Specific impulse: 330 s. Burn time: 215 s. Height: 8.40 m (27.50 ft). Diameter: 1.60 m (5.20 ft). Span: 1.80 m (5.90 ft).

Country: Ukraine. Engines: RD-857. Launch Vehicles: RT-20P. Propellants: N2O4/UDMH.
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