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LCLV-3
N2O4/UDMH propellant rocket stage. .

AKA: Low Cost Launch Vehicle. Status: Study 1968. Thrust: 2,028.04 kN (455,922 lbf). Gross mass: 161,304 kg (355,614 lb). Unfuelled mass: 19,518 kg (43,029 lb). Specific impulse: 306 s. Burn time: 210 s. Height: 15.24 m (49.99 ft). Diameter: 5.79 m (18.99 ft). Span: 5.79 m (18.99 ft).

Cost $ : 2.000 million.



Country: USA. Engines: Press Fed 200k. Launch Vehicles: LCLV. Propellants: N2O4/UDMH.

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