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R-36M ICBM



R-36M (15A14; Satan)


R-36M with different WH

WH propulsion unit

                            



 
 R-36M 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

     1.4485

 
2

 RD-0229

 1     760.0 3334

UDMH/N2O4

     0.2279  
RD-0230 4            
WH

 RD-864

 mod 4     20.20 3030

UDMH/N2O4

     0.0067  
mod     8.45 2922   0.0029

 
  First stage engine RD-264



 



 15D119 (RD-264)
  Second stage engine RD-0228 (RD-0229+RD-0230)  WH engine RD-864



   
WH propulsion unit