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R-26-2


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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 R-26-2 Nitric acid/UDMH propellant rocket stage. Orevo has sectioned hardware. TsNIIMash has 1:10 structural simulation model. All figures accurate except empty mass estimated. Source: Placard, TsNIIMash, Orevo.

AKA: 8K66. Status: Out of production. Thrust: 428.06 kN (96,232 lbf). Gross mass: 25,200 kg (55,500 lb). Unfuelled mass: 2,500 kg (5,500 lb). Specific impulse: 308 s. Specific impulse sea level: 252 s. Burn time: 160 s. Diameter: 2.40 m (7.80 ft). Span: 8.73 m (28.64 ft).

Country: Ukraine. Engines: U102-000. Launch Vehicles: R-26. Propellants: Nitric acid/UDMH. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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