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 S10E-2 stage
Part of Nova 2 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been November 1977. SSTO; expendable; payload 1,283,000 lbs.

AKA: Nova MM S10E-2. Status: Study 1963. Thrust: 160,672.00 kN (36,120,502 lbf). Gross mass: 10,302,000 kg (22,712,000 lb). Unfuelled mass: 639,000 kg (1,408,000 lb). Specific impulse: 454 s. Specific impulse sea level: 377 s. Burn time: 263 s. Height: 54.80 m (179.70 ft). Diameter: 21.30 m (69.80 ft). Span: 36.70 m (120.40 ft).

No Engines: 30.



Country: USA. Engines: CD Module. Launch Vehicles: Nova MM S10E-2. 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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use