S 5.2
Propellant:
HNO
3
/
Kerosene
Thrust:
14,918 kgf
(v)
Thrust:
13,470 kgf
(sl)
Launch vehicles:
Hwasong, Shahab, Qiam, Al-Hussein, Burkan, Paektusan-1
Nodong
Propellant:
HNO
3
/
(CH
3
)
2
NNH
2
Thrust:
28,440 kgf
(sl)
Burn time:
120 s
Launch vehicles:
Safir
First flight:
1998
Nodong
Propellant:
HNO
3
/
(CH
3
)
2
NNH
2
Thrust:
28,440 kgf
(sl)
Burn time:
120 s
Launch vehicles:
Paektusan, Uha 2
First flight:
2006
Nodong +
Propellant:
N
2
O
4
/
(CH
3
)
2
NNH
2
Thrust:
33,225 kgf
(v)
Thrust:
30,407 kgf
(sl)
Burn time:
120 s
Specific impulse:
255 s
(v)
Specific impulse:
232 s
(sl)
Launch vehicles:
Uha 3, Safir 1A, Simorgh
First flight:
2012
LRE
-
4
Propellant:
N
2
O
4
/
(CH
3
)
2
NNH
2
Thrust:
1.800 kgf
(v)
Launch vehicles:
Paektusan 2, Safir
LRE
-
4+
Propellant:
N
2
O
4
/
(CH
3
)
2
NNH
2
Thrust:
1.804 kgf
(v)
Launch vehicles:
Uha 2 / 3, Safir, Simorgh
LRE
-
15
Propellant:
N
2
O
4
/
(CH
3
)
2
NNH
2
Thrust:
3,399 kgf
(v)
Thrust:
3,749 kgf
(v)
Launch vehicles:
Simorgh
LRE
-
X
Propellant:
N
2
O
4
/
(CH
3
)
2
NNH
2
Thrust:
3,186 kgf
(v)
Launch vehicles:
Uha 2 / 3
KRE-75
Propellant:
O
2
/
Kerosene
Thrust (sl):
76,274 kgf
(v)
Thrust (sl):
66,944 kgf
(sl)
Specific impulse:
298 s
(v)
Specific impulse:
261 s
(sl)
Launch vehicles:
KSLV-2
First flight:
2022
KRE-75 vac
Propellant:
O
2
/
Kerosene
Thrust (sl):
80,710 kgf
(vl
Specific impulse:
315 s
(v)
Launch vehicles:
KSLV-2
First flight:
2022
KRE-07v
Propellant:
O
2
/
Kerosene
Thrust (sl):
6,995 kgf
(v)
Specific impulse:
325 s
(v)
Launch vehicles:
KSLV-2
First flight:
2022
RD-868
Propellant:
N
2
O
4
/
(CH
3
)
2
NNH
2
Thrust:
249 kgf
(v)
Specific impulse:
325 s
(v)
Launch vehicles:
Vega
First flight:
2012
Rutherford-1
Propellant:
O
2
/
Kerosene
Thrust (sl):
18,823 kgf
(v)
Thrust (sl):
15,652 kgf
(sl)
Specific impulse:
272 s
(sl)
Specific impulse:
327 s
(v)
Launch vehicles:
Electron
First flight:
2017
Rutherford-1 vac
Propellant:
O
2
/
Kerosene
Thrust (sl):
2,263 kgf
(v)
Specific impulse:
330 s
(v)
Launch vehicles:
Electron
First flight:
2017
