Nova B (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 B


Part of Nova


Nova B
Nova B
Credit: © Mark Wade

American heavy-lift orbital launch vehicle. Convair/Ehricke Nova design using standard tank/engine modules of 4.9 m diameter in both first and second stages; 6 F-1 engine/modules in first stage, 6 J-2 engine/modules in second stage.

Status: Study 1960. Payload: 112,000 kg (246,000 lb). Thrust: 40,024.40 kN (8,997,843 lbf). Gross mass: 2,806,400 kg (6,187,000 lb). Height: 84.00 m (275.00 ft). Diameter: 12.20 m (40.00 ft). Apogee: 556 km (345 mi).

LEO Payload: 112,000 kg (246,000 lb) to a 556 km orbit. Payload: 47,000 kg (103,000 lb) to a earth escape.

Stage Data - Nova B



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: F-1, J-2, RL-10. Stages: Nova B-1, Nova B-2, Nova B-3. Agency: Convair.



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