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
RLA-2
LOx/Kerosene propellant rocket stage. Empty mass, specific impulses, length estimated by comparison to smaller Zenit successor design.

Status: Design 1974. Thrust: 2,940.00 kN (660,930 lbf). Gross mass: 150,000 kg (330,000 lb). Unfuelled mass: 10,000 kg (22,000 lb). Specific impulse: 349 s. Burn time: 160 s. Height: 12.00 m (39.00 ft). Diameter: 6.00 m (19.60 ft). Span: 6.00 m (19.60 ft).



Country: Russia. Engines: RLA-300. Launch Vehicles: RLA-120, RLA-150, RLA-135. 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