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
N1 Block V-II
Part of N1 Block B Family
LOx/LH2 propellant rocket stage. N1 improvement study, 1965. LOx/LH2 replacement for Block B second stage.

Status: Study 1965. Thrust: 7,840.00 kN (1,762,500 lbf). Gross mass: 805,000 kg (1,774,000 lb). Unfuelled mass: 115,000 kg (253,000 lb). Specific impulse: 440 s. Burn time: 380 s. Height: 50.00 m (164.00 ft). Diameter: 10.00 m (32.00 ft). Span: 10.00 m (32.00 ft).

No Engines: 4.



Country: Russia. Engines: NK-15VM. Launch Vehicles: N-IFV-II-III, N-IMV-II-III. 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