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RLA-1


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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-1 LOx/Kerosene propellant rocket stage. Empty mass, specific impulses, length estimated by comparison to smaller Zenit successor design.

Status: Design 1974. Thrust: 11,700.00 kN (2,630,200 lbf). Gross mass: 800,000 kg (1,760,000 lb). Unfuelled mass: 45,000 kg (99,000 lb). Specific impulse: 337 s. Specific impulse sea level: 311 s. Burn time: 210 s. Height: 30.00 m (98.00 ft). Diameter: 6.00 m (19.60 ft). Span: 6.00 m (19.60 ft).

Country: Russia. Engines: RLA-1200. Launch Vehicles: RLA-120, RLA-150, RLA-135. Propellants: Lox/Kerosene. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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