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Helios C
Part of Helios LV
Helios
Helios
Helios Launch Vehicle
Credit: © Mark Wade
American nuclear-powered orbital launch vehicle.

Status: Study 1960. Payload: 86,200 kg (190,000 lb). Thrust: 10,586.00 kN (2,379,827 lbf). Gross mass: 807,440 kg (1,780,100 lb). Height: 102.00 m (334.00 ft). Diameter: 8.50 m (27.80 ft). Apogee: 556 km (345 mi).

LEO Payload: 86,200 kg (190,000 lb) to a 556 km orbit. Payload: 49,000 kg (108,000 lb) to a earth escape.

Stage Data - Helios C



Family: nuclear-powered, orbital launch vehicle. Country: USA. Engines: Helios Stage 1, Nuclear 12 Gw. Stages: Helios C-1, Helios C-2. Agency: Convair.

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