| Nova GD-2 |
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Model: Nova GD-B-2. Gross Mass: 998,000 kg (2,200,000 lb). Empty Mass: 75,000 kg (165,000 lb). Thrust (vac): 10,669.000 kN (2,398,486 lbf). Isp: 428 sec. Burn time: 357 sec. Propellants: Lox/LH2. Diameter: 20.60 m (67.50 ft). Span: 20.60 m (67.50 ft). Length: 27.10 m (88.90 ft). Country: USA. No Engines: 5. Motor: J-2. Status: Study 1963. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions. Model: Nova GD-E-2. Gross Mass: 4,535,000 kg (9,997,000 lb). Empty Mass: 363,000 kg (800,000 lb). Thrust (vac): 26,683.000 kN (5,998,577 lbf). Isp: 428 sec. Burn time: 646 sec. Propellants: Lox/LH2. Diameter: 20.60 m (67.50 ft). Span: 20.60 m (67.50 ft). Length: 47.90 m (157.10 ft). Country: USA. No Engines: 4. Motor: M-1. Status: Study 1963. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions. Model: Nova GD-F-2. Gross Mass: 1,497,000 kg (3,300,000 lb). Empty Mass: 91,000 kg (200,000 lb). Thrust (vac): 13,346.000 kN (3,000,300 lbf). Isp: 428 sec. Burn time: 435 sec. Propellants: Lox/LH2. Diameter: 18.30 m (60.00 ft). Span: 18.30 m (60.00 ft). Length: 29.90 m (98.00 ft). Country: USA. No Engines: 2. Motor: M-1. Status: Study 1963. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions. Model: Nova GD-J-2. Gross Mass: 1,270,000 kg (2,790,000 lb). Empty Mass: 91,000 kg (200,000 lb). Thrust (vac): 13,346.000 kN (3,000,300 lbf). Isp: 428 sec. Burn time: 365 sec. Propellants: Lox/LH2. Diameter: 19.50 m (63.90 ft). Span: 19.50 m (63.90 ft). Length: 38.00 m (124.00 ft). Country: USA. No Engines: 2. Motor: M-1. Status: Study 1963. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions. Used on Launch Vehicles:
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