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astronautix.com Nova GD-H

Nova Model H
Nova Model H - Nova General Dynamics Model H

Credit: © Mark Wade. 2,102 bytes. 106 x 440 pixels.



Family: Nova. Country: USA. Status: Study General Dynamics 1963.

Nova design using 1 1/2 stage arrangement and new 2.4 million kgf Lox/LH2 engines. Recoverable booster 4 engine package would separate at 2,980 m/s at 87,800 m altitude; splashdown under 4 46 m diameter parachutes 1,000 km downrange. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions.


Specifications

LEO Payload: 454,000 kg. to: 185 km Orbit. at: 0.0 degrees. Liftoff Thrust: 11,789,750 kgf. Total Mass: 9,365,800 kg. Core Diameter: 25.9 m. Total Length: 89.0 m.



Bibliography:



Nova  - GDNova - GD - Nova Concepts - General Dynamics

Credit: © Mark Wade. 11,186 bytes. 641 x 351 pixels.



Nova GD AdvancedNova GD Advanced - General Dynamics advanced Nova designs

Credit: Lockheed Martin. 23,896 bytes. 527 x 373 pixels.



Nova Model H CutawayNova Model H Cutaway - Nova General Dynamics Model H Cutaway

Credit: © Mark Wade. 4,943 bytes. 260 x 440 pixels.



Nova F, H and JNova F, H and J - Cutaway view of General Dynamics Nova F, H and J concepts.

Credit: Lockheed Martin. 30,423 bytes. 536 x 412 pixels.



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Last update 12 March 2001.
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