Monoblock UR-500-2
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
N2O4/UDMH propellant rocket stage. Original Proton second stage design.
No Engines: 4.
Subtopics
- 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.
Related
- Country
- Russia
- Engines
- RD-0213
- Launch Vehicles
- Monoblock UR-500, Polyblock UR-500
- Propellants
- N2O4/UDMH