Vysota-1 (original) (raw)

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Vysota-1

Part of R-29-1

N2O4/UDMH propellant rocket stage.

Status: Retired 1996. Thrust: 682.00 kN (153,319 lbf). Gross mass: 20,000 kg (44,000 lb). Burn time: 74 s. Height: 7.70 m (25.20 ft). Diameter: 1.90 m (6.20 ft).

Country: Russia. Engines: RD R-29 (1). Launch Vehicles: Vysota. Propellants: N2O4/UDMH. Agency: Makeyev bureau.

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