The Wayback Machine - https://web.archive.org/web/20161228051812/http://astronautix.com/z/zenit-b.html
Zenit-B

Encyclopedia Astronautica
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

Zenit-B
Zenit stage 2. LOx/Kerosene propellant rocket stage.

AKA: Zenit-2. Status: Active. Thrust: 912.00 kN (205,025 lbf). Gross mass: 90,600 kg (199,700 lb). Unfuelled mass: 9,000 kg (19,800 lb). Specific impulse: 349 s. Burn time: 315 s. Height: 11.50 m (37.70 ft). Diameter: 3.90 m (12.70 ft). Span: 3.90 m (12.70 ft).

Cost $ : 15.000 million.

Country: Ukraine. Engines: RD-120. Launch Vehicles: Zenit-2, Zenit-2 11K77.05, Zenit-3SL, Zenit-2M, Zenit-3SLB. Propellants: Lox/Kerosene.



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
� 1997-2016 Mark Wade - Contact
� / Conditions for Use