Propulsion Paektusan


      
   
Nodong engine generate 32 t of thrust (vac)


Single second stage engine LRE-4 (Paektusan-2)

Paektusan-1 (Nodong based)

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

Nodong  (1)*

279.8 2383 308.5 2628 11.151 95 0.1174 29.4
2

Isayev S5.2

    116.3 2530 4.34 75 0.0460 11.0
3

solid fuel

    44.5 2314 0.52 27 0.0192 1.2

Paektusan-2 (Nodong++ based)

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

Nodong    (1)*

284.4 2422 313.2 2667 18.20 155 0.1174 48.6
2

LRE-4      (2)

    34.1 2736 3.05 245 0.0124 8.3


*
Nodong (= R-17K engine)


This scheme was found on the captured freighter "Kuwolsan"
A Scud or Nodong engine + control engines