OK-M2

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OK-M2

Part of OK

OKM-2 Spaceplane

Russian manned spaceplane. Study 1984. The OK-M2 was a manned spaceplane, a straight delta wing joined to a broad fuselage with an upturned nose.

Status: Study 1984. Payload: 10,000 kg (22,000 lb). Thrust: 79.40 kN (17,850 lbf). Gross mass: 30,000 kg (66,000 lb). Unfuelled mass: 27,300 kg (60,100 lb). Height: 15.00 m (49.00 ft). Span: 10.00 m (32.00 ft).

The OK-M2 was designed by NPO Molniya as a follow-on to the OK-M of NPO Energia with less development cost and risk than Energia's proposed OK-M1 / MMKS shuttle system.

Crew Size: 8.

Family: Space station orbit, Spaceplane. Country: Russia. Launch Vehicles: Energia, Energia M. Propellants: N2O4/UDMH. Agency: Molniya bureau. Bibliography: 89.

Photo Gallery

OKM-2 Booster

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