| astronautix.com | Nova GD-H |
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| Nova Model H - Nova General Dynamics Model H Credit: © Mark Wade. 2,102 bytes. 106 x 440 pixels. |
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.
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.
![]() | Nova - GD - Nova Concepts - General Dynamics Credit: © Mark Wade. 11,186 bytes. 641 x 351 pixels. |
![]() | Nova GD Advanced - General Dynamics advanced Nova designs Credit: Lockheed Martin. 23,896 bytes. 527 x 373 pixels. |
![]() | Nova Model H Cutaway - Nova General Dynamics Model H Cutaway Credit: © Mark Wade. 4,943 bytes. 260 x 440 pixels. |
![]() | Nova 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. |