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R-36MU ICBM (>Dnepr)



R-36MU (15A18; Satan)


Dnepr (right) is a R-36MU with R-36M2 upper stage
and PBV/fairing change

 
 R-36MU ICBM Thrust s.l. Isp s.l. Thrust vac Isp vac

Propellant

Burn time

Flow rate

Total Imp.(vac)

 Stage

Engines

 Chamb.

kN Ns/kg kN Ns/kg

Fuel/Oxidizer

tons

sec

t/sec

MN*sec

1

 RD-264

 4 x 1 4,166.3 2876 4,522.8 3122

UDMH/N2O4

147.90 ~102 1.4485

461.8

2

 RD-0229

1     760.0 3334

UDMH/N2O4

36.75 ~161 0.2279 122.5
RD-0230 4     ? ? ?
PBV

 RD-869

mod 4     20.21 3069

UDMH/N2O4

    0.0066  
mod     8.28 2964   0.0028

 

  First stage engine RD-264   Second stage engine RD-0229 (RD-0230)



  

  PBV engine RD-869