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LCLV-1
N2O4/UDMH propellant rocket stage. .

AKA: Low Cost Launch Vehicle. Status: Study 1968. Thrust: 56,368.00 kN (12,672,030 lbf). Gross mass: 3,253,246 kg (7,172,179 lb). Unfuelled mass: 396,013 kg (873,059 lb). Specific impulse: 267 s. Specific impulse sea level: 245 s. Burn time: 130 s. Height: 39.33 m (129.03 ft). Diameter: 12.20 m (40.00 ft). Span: 12.20 m (40.00 ft).

Cost $ : 30.000 million.



Country: USA. Engines: Press Fed 5748k. Launch Vehicles: LCLV. Propellants: N2O4/UDMH.

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