BUILDER(S)
Prime contractor:
The 4th Machine Industry Bureau, Pyongyang, North Korea
Subcontractors:
No. 26 General Plant, Kanggye, North Korea (missile subcontractor)
Changgwang Sinyong Corp., Pyongyang, North Korea (exporter)
May also be in domestic production in Iran.
USERS/PLATFORMS
Iran [N/A]
North Korea [10] (No Dong 1/2) (estimates vary widely)
CHARACTERISTICS
No Dong MRBM
WEIGHTS
Launch 35,825 lb (16,250 kg)
Warhead 2,553 lb ( 1,158 kg)
DIMENSIONS
Length 52 ft 6 in (16.00 m)
Diameter 4 ft 4 in ( 1.32 m)
Configuration cylinder with tapered nosecone, slightly
smaller diameter cylinder at rear of
missile, 4 clipped delta tail fins
PROPULSION
Engine single-stage 1-chamber liquid-propellant
rocket
Thrust 58,643 lb (26,600 kg)
Fuel TM-185
Oxidizer AK-27I
Propellant mass 28,466 lb (12,912 kg)
PERFORMANCE
Range 729 nm (839 mi, 1,350 km)
CEP 208 yd (190 m)
Launch preparation 60 min
Burn time 110 sec
Deployment mobile
WARHEAD
Nuclear possible, but type unknown
Chemical thickened VX
Conventional 2,553 lb (1,158 kg) HE
GUIDANCE
Type inertial
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