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
Ikar stage
N2O4/UDMH propellant rocket stage. Derived from propulsion module of Yantar spy satellite, over 30 flights to 1998. 50 restarts.
Status: Active. Thrust: 2.94 kN (661 lbf). Gross mass: 3,164 kg (6,975 lb). Unfuelled mass: 820 kg (1,800 lb). Specific impulse: 326 s. Burn time: 600 s. Height: 2.56 m (8.39 ft). Diameter: 2.72 m (8.92 ft). Span: 2.72 m (8.92 ft).
Ikar upper stage upgrades the Soyuz LV, replaces Block L; increased versatility due to capability for 50 restarts. Engine thrusts: 1 x 2943 N + 4 x 110 N + 4 x 52 N + 8 x 5.88 N.
Family:
Space Tugs.
Country:
Russia.
Engines:
17D61.
Launch Vehicles:
Soyuz 11A511U / Ikar.
Propellants:
N2O4/UDMH.
Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use