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 R10E-2 stage
Part of Nova 2 stage series Family
Air/LOx/LH2 propellant rocket stage. Operational date would have been October 1980. Expendable stage. Air-augmented plug nozzle.

AKA: Nova MM R10E-2. Status: Study 1963. Thrust: 140,539.00 kN (31,594,424 lbf). Gross mass: 8,474,000 kg (18,681,000 lb). Unfuelled mass: 1,188,000 kg (2,619,000 lb). Specific impulse: 620 s. Specific impulse sea level: 620 s. Burn time: 310 s. Height: 49.10 m (161.00 ft). Diameter: 21.30 m (69.80 ft). Span: 43.70 m (143.30 ft).

No Engines: 40.



Country: USA. Engines: CD Module. Launch Vehicles: Nova MM R10E-2. Propellants: Air/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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use