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Atlas LV-3B
Part of Atlas Family
American orbital launch vehicle. First operational version of Atlas ICBM and used as launch vehicle for Project Mercury.

AKA: LV-3B. Status: Out of production. Payload: 1,360 kg (2,990 lb). Thrust: 1,587.20 kN (356,817 lbf). Gross mass: 117,730 kg (259,550 lb). Height: 25.00 m (82.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 1,360 kg (2,990 lb) to a 185 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 14.210 million. Maximum range: 13,000 km (8,000 mi).



Family: orbital launch vehicle. Country: USA. Agency: Convair.

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