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Nova A-1
Part of Nova 1 stage series
Nova A Credit: © Mark Wade |
LOx/Kerosene propellant rocket stage. .
Status: Study 1960. Thrust: 30,616.00 kN (6,882,750 lbf). Gross mass: 1,342,000 kg (2,958,000 lb). Unfuelled mass: 73,000 kg (160,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 121 s. Height: 28.00 m (91.00 ft). Diameter: 9.80 m (32.10 ft). Span: 11.90 m (39.00 ft).
No Engines: 4.
Country:
USA.
Engines:
F-1.
Launch Vehicles:
Nova C,
Nova A.
Propellants:
Lox/Kerosene.
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