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 1C-1
Part of Nova 1 stage series
LOx/Kerosene propellant rocket stage. Operational date would have been February 1973.

Status: Study 1963. Thrust: 161,710.00 kN (36,353,850 lbf). Gross mass: 8,943,000 kg (19,715,000 lb). Unfuelled mass: 590,000 kg (1,300,000 lb). Specific impulse: 304 s. Specific impulse sea level: 271 s. Burn time: 151 s. Height: 49.70 m (163.00 ft). Diameter: 21.00 m (68.00 ft). Span: 27.10 m (88.90 ft).

No Engines: 18.



Country: USA. Engines: F-1A. Launch Vehicles: Nova MM 1C. Propellants: Lox/Kerosene.

Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use