Photo Gallery
MR-UR-100U ICBM
Second stage with unknown engines 15A1/15A1V
Propellant
Burn time
Flow rate
Total Imp.(vac)
Engines
Chamb.
Fuel/Oxidizer
tons
sec
t/sec
MN*sec
RD-268
UDMH/AK-27
0.1072
15A1
4 (?)
Second stage engine 15A1 (15A1V)
Note: the whole thing is rather uncertain