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Sanger I-2
LOx/LH2 propellant rocket stage. The second stage would reach a 300 km earth orbit and a top speed of 8000 m/s. The glider had a landing speed of 90 m/s. Aside from the two-man crew, a five metric ton payload could be delivered into orbit.

Status: Study 1965. Thrust: 295.00 kN (66,318 lbf). Gross mass: 21,000 kg (46,000 lb). Unfuelled mass: 5,000 kg (11,000 lb). Specific impulse: 430 s. Burn time: 220 s. Height: 20.50 m (67.20 ft). Diameter: 2.20 m (7.20 ft). Span: 8.80 m (28.80 ft).



Country: Germany. Propellants: Lox/LH2.

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