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
EKR Stage 1
Part of R-17 Family
LOx/Kerosene propellant rocket stage. First stage for Eksperimentalnaya krilataya raketa (experimental winged rocket), Mach 3 ramjet. Boosted second stage to ramjet ignition conditions.

Status: Study 1953. Thrust: 107.33 kN (24,129 lbf). Gross mass: 6,390 kg (14,080 lb). Unfuelled mass: 1,564 kg (3,448 lb). Specific impulse: 250 s. Specific impulse sea level: 217 s. Burn time: 127 s. Height: 8.29 m (27.19 ft). Diameter: 0.88 m (2.88 ft). Span: 3.06 m (10.05 ft).



Country: Russia. Engines: S2.253 derivative. Launch Vehicles: EKR. 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