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 A-1
Part of Nova 1 stage series
Nova A
Nova A
Credit: © Mark Wade
LOx/Kerosene propellant rocket stage. .

Status: Study 1960. Thrust: 30,616.00 kN (6,882,750 lbf). Gross mass: 1,342,000 kg (2,958,000 lb). Unfuelled mass: 73,000 kg (160,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 121 s. Height: 28.00 m (91.00 ft). Diameter: 9.80 m (32.10 ft). Span: 11.90 m (39.00 ft).

No Engines: 4.



Country: USA. Engines: F-1. Launch Vehicles: Nova C, Nova A. Propellants: Lox/Kerosene.

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