Nova GD-B

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Nova GD-B

Nova Model B - Nova General Dynamics Model B

Credit: © Mark Wade. 1,726 bytes. 93 x 444 pixels.

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

Nova design using existing engines. Recoverable engine package; separation at 3,398 m/s at 76,200 m altitude; splashdown using retrorockets under 7 30 m diameter parachutes 1300 km downrange. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions.

Specifications

LEO Payload: 338,000 kg. to: 185 km Orbit. at: 0.0 degrees. Liftoff Thrust: 12,698,540 kgf. Total Mass: 10,473,600 kg. Core Diameter: 20.6 m. Total Length: 87.0 m.

Stage Number: 1. 1 x Nova GD-B-1 Gross Mass: 9,070,000 kg. Empty Mass: 635,000 kg. Thrust (vac): 14,526,000 kgf. Isp: 310 sec. Burn time: 177 sec. Isp(sl): 271 sec. Diameter: 20.6 m. Span: 25.7 m. Length: 45.2 m. Propellants: Lox/Kerosene No Engines: 16. F-1A
Stage Number: 2. 1 x Nova GD-B-2 Gross Mass: 998,000 kg. Empty Mass: 75,000 kg. Thrust (vac): 1,088,000 kgf. Isp: 428 sec. Burn time: 357 sec. Diameter: 20.6 m. Span: 20.6 m. Length: 27.1 m. Propellants: Lox/LH2 No Engines: 5. J-2

Bibliography:

215 - Scala, Keith J, and Swanson, Glen E, Quest, "They Might Be Giants Part 1", Fall, 1992.

Nova B and E - Cutaway view of General Dynamics Nova B and E concepts.

Credit: Lockheed Martin. 27,549 bytes. 536 x 385 pixels.

Nova Model B Cutaway - Nova General Dynamics Model B Cutaway

Nova GD Advanced - General Dynamics advanced Nova designs

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

Nova - GD - Nova Concepts - General Dynamics

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Last update 12 March 2001.
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© Mark Wade, 2001 .