Sanger I-1

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Sanger I-1

LOx/LH2 propellant rocket stage. The first stage took the second stage to 50 km altitude and 4000 m/s separation conditions. The first stage would then land 500 km from the launch point. Takeoff speed was 300 m/s; and landing speed 80 m/s. A two-man crew piloted the booster.

Status: Study 1965. Thrust: 885.00 kN (198,955 lbf). Gross mass: 79,000 kg (174,000 lb). Unfuelled mass: 10,000 kg (22,000 lb). Specific impulse: 430 s. Specific impulse sea level: 330 s. Burn time: 300 s. Height: 31.00 m (101.00 ft). Diameter: 3.35 m (10.99 ft). Span: 11.80 m (38.70 ft). Location: 4000.

No Engines: 3. Release velocity: 4,000 m/s (13,100 ft/sec). Release altitude: 50,000 m (164,000 ft).

Country: Germany. Propellants: Lox/LH2.

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