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Viking-1
LOx/Alcohol rocket stage. 93.00 kN (20,907 lbf) thrust. Mass 4,500 kg (9,921 lb).

Status: Retired 1957. Thrust: 93.00 kN (20,907 lbf). Gross mass: 4,500 kg (9,900 lb). Unfuelled mass: 800 kg (1,760 lb). Burn time: 70 s. Height: 14.90 m (48.80 ft). Diameter: 0.81 m (2.65 ft).


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Viking Type 9-1 LOx/Alcohol rocket stage. 93.00 kN (20,907 lbf) thrust. Mass 6,800 kg (14,991 lb).

Country: USA. Engines: NRL Viking. Launch Vehicles: Viking sounding rocket. Propellants: Lox/Alcohol. Agency: Martin. Bibliography: 13343.

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