Nova 2 F-1 Module

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 2 F-1 Module

Part of Nova 2 stage series

Nova NASA 8 F-1
Nova NASA 8 F-1 Modular
Credit: © Mark Wade

LOx/Kerosene propellant rocket stage. Short Nova building block. Four used in stage 1, one in stage 2.

Status: Study 1960. Thrust: 15,121.00 kN (3,399,336 lbf). Gross mass: 1,134,000 kg (2,500,000 lb). Unfuelled mass: 77,000 kg (169,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 200 s. Height: 28.70 m (94.10 ft). Diameter: 10.10 m (33.10 ft). Span: 10.10 m (33.10 ft).

No Engines: 2.

Country: USA. Engines: F-1. Launch Vehicles: Nova 8L Mod. Propellants: Lox/Kerosene.

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