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-A
RD-170
RD-170
Credit: © Mark Wade
LOx/Kerosene propellant rocket stage. Modification of same stage used as strap-on for Energia launch vehicle.

AKA: Zenit-1. Status: Active. Thrust: 8,181.13 kN (1,839,191 lbf). Gross mass: 354,300 kg (781,000 lb). Unfuelled mass: 28,600 kg (63,000 lb). Specific impulse: 337 s. Specific impulse sea level: 311 s. Burn time: 150 s. Height: 32.90 m (107.90 ft). Diameter: 3.90 m (12.70 ft). Span: 3.90 m (12.70 ft).

Cost $ : 30.000 million.



Subtopics

Energia Strapon LOx/Kerosene propellant rocket stage. Essentially identical to Zenit stage 1.

Country: Ukraine. Engines: RD-171. 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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use