Engines Proton


           
  RD-253 (Mk-1)                                           RD-253 (Mk-2)                                                    RD-253 (Mk-3)                                               RD-253 (Mk-4)

 
      
RD-0208/0209                                      RD-0210/0211      


    
RD-0213/0214 (=RD-0212)                                    RD-0213                  

 

Stage

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp

  -

 -

kN

N*s/kg

kN

N*s/kg

tons

s

t/s

MN*s
1

RD-253 (6)

 UR-500 8,386.5 2790 9,271.5 3094 419,41 140 2.9966 1,297.6

Mk-1

 8,681.7 2792 9,630.1 3097 419.41 134.9 3.1096

1,298.9

Mk-2

 8,840.9 2792 9,806.8 3097 419.41 132.5 3.1666

1,298.9

Mk-3

 9,194.6 2796 10,184.5 3097 419.41 127.5 3.2886 1,298.9
Mk-4 9,468.6 2796 10,487.9 3097 419.41 123.8 3.3866 1,298.9

RD-275 (6)

Mk-5

 9,548.2 2819 10,487.9 3097 419.41 123.8 3.3866 1,298.9
2

RD-0208/
RD-0209 (1+3)

UR-500

     2,296.2 3207 121.72 170 0.7160 390.3

RD-0210 /
RD-0211(1+3)

 Mk-1...Mk-2     2,352.0 3210 156.11 213 0.7328 501.1
Mk-3...Mk-5     2,400.0 3210 156.11 208.8 0.7477 501.1

3

RD-0213

 Mk-1...Mk-2     581.8 3200 43.86 241.3 0.1818 148.1
Mk-3...Mk-5     594.0 3200 43.86 236.3 0.1856 148.1

+ RD-0214 (4)

 

  

30.9

2870

 2.70

250

 0.0108

 

 

Second stage with RD-0210/0211


  
RD-58M (11D58M)

Block-D

Version

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp

  -

 -

kN

N*s/kg

kN

N*s/kg

tons

s

t/s

MN*s

D

 RD-58     83.36 3422 11.45 470 0.0244 39.2
D-1     83.36 3452 12.56 520 0.0242 43.3
D-2     83.36 3452 14.97 620 0.0242 51.7
DM RD-58M     83.61 3462 15.22 630 0.0242 52.7
Dm1     83.61 3462 15.22 630 0.0242 52.7
DM-2     83.61 3462 15.46 640 0.0242 53.5
Dm2     83.61 3462 15.46 640 0.0242 53.5
DM-2M     83.61 3462 15.94 660 0.0242 55.2
DM-3     83.61 3462 16.42 680 0.0242 56.9
Dm4     83.61 3462 15.46 640 0.0242 53.5
Dm5     83.61 3462 15.46 640 0.0242 53.5