RT-23-3 (original) (raw)


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


RT-23-3


N2O4/UDMH propellant rocket stage.

Status: Retired 1998. Thrust: 206.00 kN (46,310 lbf). Gross mass: 15,000 kg (33,000 lb). Height: 3.60 m (11.80 ft). Diameter: 2.40 m (7.80 ft).



Country: Russia. Engines: RD-866. Launch Vehicles: RT-23 15Zh44, RT-23U 15Zh60, RT-23 15Zh52, RT-23U 15Zh61. Propellants: N2O4/UDMH. Agency: Yuzhnoye.



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