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| Nova Douglas 2 - Nova Douglas Aircraft Model 2 Credit: © Mark Wade. 1,465 bytes. 81 x 416 pixels. |
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Family: Nova. Country: USA. Status: Study 1963.
Douglas/Bono design for Nova using LH2/Lox in both stages.
SpecificationsLEO Payload: 454,500 kg. to: 325 km Orbit. at: 0.0 degrees. Liftoff Thrust: 8,777,300 kgf. Total Mass: 7,121,400 kg. Core Diameter: 21.3 m. Total Length: 124.0 m.
- Stage Number: 1. 1 x Nova DAC 2-1 Gross Mass: 4,943,000 kg. Empty Mass: 311,000 kg. Thrust (vac): 10,431,000 kgf. Isp: 410 sec. Burn time: 179 sec. Isp(sl): 345 sec. Diameter: 21.3 m. Span: 21.3 m. Length: 82.3 m. Propellants: Lox/LH2 No Engines: 15. M-1
- Stage Number: 2. 1 x Nova DAC 2-2 Gross Mass: 1,633,000 kg. Empty Mass: 113,000 kg. Thrust (vac): 1,361,000 kgf. Isp: 426 sec. Burn time: 468 sec. Diameter: 21.3 m. Span: 21.3 m. Length: 21.3 m. Propellants: Lox/LH2 No Engines: 4. M-1
Bibliography:- 214 - Bono, Philip, Advanced in the Astronautical Sciences, "Design Objectives for Tomorow's Big Boosters", 1963.
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