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LCLV-2
N2O4/UDMH propellant rocket stage. .

AKA: Low Cost Launch Vehicle. Status: Study 1968. Thrust: 9,793.30 kN (2,201,622 lbf). Gross mass: 798,389 kg (1,760,146 lb). Unfuelled mass: 95,092 kg (209,641 lb). Specific impulse: 300 s. Burn time: 210 s. Height: 25.91 m (85.00 ft). Diameter: 9.15 m (30.01 ft). Span: 9.15 m (30.01 ft).

Cost $ : 8.000 million.



Country: USA. Engines: Press Fed 1000k. Launch Vehicles: LCLV. Propellants: N2O4/UDMH.

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