Nova GD-J (original) (raw)


Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z


Nova GD-J


Part of Nova


Nova Model J Cutaway
Nova Model J Cutaway
Nova General Dynamics Model J Cutaway
Credit: © Mark Wade

American heavy-lift orbital launch vehicle. General Dynamics Nova design using recoverable LOx/RP-1 stage of ballistic shape with 3 million kgf engines; separation at 3,420 m/s at 93,900 m altitude; splashdown using retrorockets under 7 parachutes 1340 km downrange. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions.

Status: Study 1963. Payload: 454,000 kg (1,000,000 lb). Thrust: 116,526.40 kN (26,196,177 lbf). Gross mass: 10,431,800 kg (22,998,100 lb). Height: 90.00 m (295.00 ft). Diameter: 42.40 m (139.10 ft). Apogee: 185 km (114 mi).

LEO Payload: 454,000 kg (1,000,000 lb) to a 185 km orbit.

Stage Data - Nova GD-J



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: L-6.55, M-1. Stages: Nova GD-J-1, Nova GD-J-2. Agency: Convair.


Photo Gallery



Nova GD Advanced Nova GD AdvancedGeneral Dynamics advanced Nova designsCredit: Lockheed Martin


Nova  - GD Nova - GDNova Concepts - General DynamicsCredit: © Mark Wade


Nova F, H and J Nova F, H and JCutaway view of General Dynamics Nova F, H and J concepts.Credit: Lockheed Martin


Nova Model J Nova Model JNova General Dynamics Model JCredit: © Mark Wade



Back to top of page


Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z


© 1997-2019 Mark Wade - Contact
© / Conditions for Use