Burlak Stage 1
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
N2O4/UDMH propellant rocket stage. Masses, thrust, specific impulse estimated based on total vehicle mass of 28.5 metric tons and first stage burn time of 140 seconds. Air launched from Tu-160 at 13,500 m, Mach 1.7 release conditions.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- Burlak
- Propellants
- N2O4/UDMH
- Stages
- Burlak Stage 1