Nova MM T10RR-3-2

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 MM T10RR-3-2

Part of Nova 2 stage series

LOx/LH2 propellant rocket stage. Operational date would have been July 1977. Recoverable stage.

Status: Study 1963. Thrust: 12,052.00 kN (2,709,397 lbf). Gross mass: 1,229,000 kg (2,709,000 lb). Unfuelled mass: 136,000 kg (299,000 lb). Specific impulse: 454 s. Burn time: 397 s. Height: 21.80 m (71.50 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).

No Engines: 2.

Country: USA. Engines: CD Module. Launch Vehicles: Nova MM T10RR-3. 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