SLS Stage C

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

SLS Stage C

Part of Nova 3 stage series

LOx/LH2 propellant rocket stage. Launch vehicle core stage for Project Lunex. Masses estimated based on optimum apportioning of B+C stage total masses. Thrust, engines estimated based on requirements.

Status: Study 1961. Thrust: 10,673.32 kN (2,399,458 lbf). Gross mass: 825,000 kg (1,818,000 lb). Unfuelled mass: 58,000 kg (127,000 lb). Specific impulse: 428 s. Burn time: 350 s. Height: 53.00 m (173.00 ft). Diameter: 7.62 m (24.99 ft). Span: 7.62 m (24.99 ft).

No Engines: 2.

Country: USA. Engines: M-1. Launch Vehicles: SLS BC-2720. Propellants: Lox/LH2.

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