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Missiles

Name Stages Propellant Range (km) IOC Inventory Type Body Dia. (m) Comments
Scud-B 1 liquid 280-330 1981 100? SRBM 0.885  
Hwasong-5 1 liquid 280-330 1984 150? SRBM 0.885 Derivative of Scud-B
Hwasong-6 1 liquid 500-700 1989 250? SRBM 0.885 Derivative of Scud-C
No-dong 1 liquid 1,350-1,500 1999 12-36 MRBM 1.3 Also flown by Iran (Shahab-3) and Pakistan (Ghauri II)
Taep'o-dong-1 Paeutudan-1 2 liquid 2,000-2,200 2000 0 MRBM 1.3 Indigenously developed system with performance similar to the Soviet SS-4
NKSL-1/Taep'o-dong-1 3 liquid + solid 2,200-2,672
or
2,200-2,896
1998
(ILC)
0 M/IRBM 1.3 Satellite launch variant of the Taep'o-dong-1. Basis for the design of Iran's Shahab-4
Taep'o-dong-2 2 liquid 3,500-3,750
6,400-6,700
7,000
8,000-12,000
N/A 0 LRICBM
LRICBM
LRICBM
FRICBM
2.2 This is a hypothetical advance on the Taep'o-dong-1. North Korea is not believed to currently possess a functional version of this missile, but both North Korea and Iran (Shahab-5) are believed to be working towards a missile with these capabilities.
NKSL-X-2/Taep'o-dong-2 3 liquid + solid 4,000-4,300 N/A
(ILC)
0 LRICBM 2.2 This is a satellite launch variant of the hypothetical Taep'o-dong-2 model that may be under development. Basis for the design of Iran's Shahab-6. It would probably have a similar performance to the Soviet SS-5

No-dong / Shahab-3
Range-Payload to Throwweight Trade-offs
Stages Payload Range Country
kg Pounds km Miles
One-Stage 1,158 2,553 1,350 839 Iran
760 1,676 1,500 932 Pakistan
Official figures
Taep'o-dong-1 / Shahab-4
Range to weight Defenition
Stages Payload Range
kg Pounds km Miles
Two-Stage 1,000 2,205 2,000 1,243
750 1,654 2,200 1,367
Three-Stage 500 1,103 2,475 1,538
380 838 2,672 1,660
290 640 2,896 1,800
Estimates based on limited data
Taep'o-dong-2 / Shahab-5
Range-Payload to Throwweight Trade-offs
Stages Payload Range
kg Pounds km Miles
Two or Three
Stage variant
1,000 2,205 3,500 2,175
750 1,654 3,750 2,330
570 1,257 4,000 2,486
500 1,103 4,100 2,548
420 926 4,248 2,640
403 889 4,264 2,650
390 860 4,300 2,672
Estimates based on limited data
Improved Taep'o-dong-2B / Shahab-5B/6
Range to weight Defenition
Stages Payload Range
kg Pounds km Miles
Three-Stage 610-490 1,345-1081 5470 3,399
570-480 1,257-1058 5,500 3,418
490-440 1,080-970 5,632 3,500
290-330 640-728 6,000 3,728
230-270 505-595 6,200 3,853
170-220 375-485 6,400 3,977
100-150 221-331 6,700 4,163
Preliminary Estimates based on limited data (March 2002)
Taep'o-dong-3 / Shahab-5B / 6
Range to weight Defenition
Stages Payload Range
kg Pounds km Miles
Three-Stage 1,200-1,220 2,646-2,690 5,470 3,399
1,130-1,200 2,492-2,646 5,500 3,418
900-1,040 2,492-2,646 5,500 3,418
700 1,544 6,000 3,728
550-540 1,213-1,191 6,200 3,853
390-420 860-926 6,400 3,977
270-290 595-640 6,700 4,163
Preliminary Estimates based on limited data (March 2002)
Taep'o-dong-4 / Shahab-7 Concepts
Range to weight Defenition
Stages Payload Range
kg Pounds km Miles
Three-Stage 1,030 2,271 9,000 5,593
810 1,786 10,000 6,214
480 1,054 12,000 7,457
100 221 15,000 9,321
Preliminary Estimates based on a conceptual model for the system

NOTES:

SRBM - Short Range Ballistic Missile < 1,000 km
MRBM - Medium Range Ballistic Missile 1,000-2,500 km
IRBM - Intermediate Range Ballistic Missile 2,500-3,500 km
LRICBM - Limited Range Intercontinental Ballistic Missile 3,500-8,000 km

Many of the ranges suggested for the yet-to-fly missile systems are based on mathematical models relying on what little data has been made public. The large ranges suggested by some of these studies do not necessarily imply likely ranges for an armed missile in the near future, rather they often attempt to extrapolate a maximum possible range for a given design, so as to come up with a worst-case scenario.



Sources and Resources



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