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
Monoblock UR-500-2
AKA: UR-500 Stage 2. Status: Design 1962. Thrust: 3,183.20 kN (715,612 lbf). Gross mass: 137,700 kg (303,500 lb). Unfuelled mass: 16,000 kg (35,000 lb). Specific impulse: 320 s. Burn time: 119 s. Height: 10.90 m (35.70 ft). Diameter: 4.10 m (13.40 ft). Span: 4.10 m (13.40 ft).
No Engines: 4.
| UR-500-2 N2O4/UDMH propellant rocket stage. Proton UR-500 second stage. Flew only on two-stage version of Proton. Empty mass is correct; all other values estimated based on UR-500 Stage 2 original design and UR-500K stage 2 figures. |
| Proton K-2 Proton K stage 2. |
| UR-500MK-2 LOx/Kerosene propellant rocket stage. Empty mass estimated based on overall vehicle mass fraction. Length estimated based on total mass. |
Country: Russia. Engines: RD-0213. Launch Vehicles: Monoblock UR-500, Polyblock UR-500. 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