NoDong




Basic Data
Mission medium-range ballistic missile
Developed by North Korea
Deployed by Iran, North Korea, Libya, Pakistan, Syria Service North Korean Air Force
Development Year 1988
Deployment Year 1993
Targets US armed force bases in Japan and Japanese cities, military sites
Platform modified MAZ 543 REL
Number manufactured 75-150 missiles(by end of 1999), 24-50 exported, 50-100 in inventry
Number deployed 200
Design The 4th Machine Industry Bureau
Manufacturer The underground facility at the No.26 General Plant, Kanggye

Specification / Performance
Length 16.0m
Body Diameter 1.32m
Wing/Fin span 2.58m
Launch Weight 16,250kg
Range 1,350km(payload: 1,200kg), 1,500km(payload: 700kg)
Accuracy 2,000-4,000m CEP

Subsystems
Propulsion 1-stage liquid fuel rocket motor
Engine 4xScud-engine (cluster), a thrust of about 50,000kgf, burn time: 95sec
Payload single warhead 700-1,200kg
Warhead conventional HE, chemical(nerve gas), biological, submunition(100 5kg bomblets) or nuclear(50kT)
Guidance Strap-Down to Inertial with GPS

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DF-15(East Wind-15)/M-9 USA name
CSS-6



Basic Data
Mission short-range road-mobile ballistic missile
Developed by China
Deployed by China, Libya, Syria, Iran, Pakistan
Service Chinese Second Artillery
Development Year 1985
Deployment Year 1989
Targets targets along China's border, including Taiwan
Platform a 8X8 transporter-erector-launcher (TEL) vehicle(TAS5380)
Number deployed 150( as of Feb 1999), 650( as of 2005)
Contractor Chinese State Factories, Marketing: CPMIEC(Beijing)
Design CASC China Academy of Rocket Motor Technology (ARMT, also known as 4th Aerospace Academy)
Unit cost $2,000,000(est.)

Specification / Performance
Length 9.1m
Body Diameter 1.0m
Launch Weight 6,200kg
Range 200-600km(800km for small warhead)
Accuracy 150-500m CEP

Subsystems
Propulsion 1-stage solid-fuel rocket motor
Payload single warhead 500kg
Warhead HE or 50-350kT nuclear, chemical, submunition or fuel-air explosive
Guidance inertial, terminal control (by GPS/INS?)

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Deployed by Belarus, Czech Rep., Germany, Hungary, Kazakhstan, Poland, Russia, Slovakia, Syria, Ukraine, Yemen
Service Russian Army
Deployment Year 1976(A), 1986(B)
Targets critical targets deep within enemy battle formations
Platform 9P129 TEL: 6 wheeled modified ZIL-5937 or BAZ5921(9P129) TEL
Number deployed about 300 TEL (in RUSSIA), 200 missiles were built each year.About 1,200 missiles (as of 1993)(310 nuclear warheads)
Design Nepobidimy Design Bureau
Manufacturer Petropavlovsk Machine Plant,Ukraine(9M79 missile),Lenin Heavy Machine Plant,Kazakhstan(9P129 launch system)
Unit cost $1,700,000(9M79M-1 missile), $3,300,000(9P128M1 TEL launch vehicle)

Specification / Performance
Length 6.4m
Body Diameter 65cm
Launch Weight 2,000kg(Tochka), 2,010kg(Tochka-U)
Range 15-70km(Tochka), 20-120km(Tochka-U)
Accuracy 50-100m CEP

Subsystems
Propulsion 1-stage solid-fuel rocket motor
Payload single warhead 482kg
Warhead 10 or 100kT nuclear,HE,chemical or submunition
Guidance inertial (passive radar terminal option)

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R-17 Elbrus USA/NATO name
SS-1c Scud B



Basic Data
Mission short-range ballistic missile
Developed by Soviet Union
Deployed by Afghanistan, Algeria, Azerbaijan, Belarus, Bulgaria, Czech, Egypt, Georgia, Hungary, Iran, Iraq, Kazakhstan, Libya, North Korea, Poland, Romania, Serbia, Slovakia, Soviet Union, Syria, Yemen
Service Soviet Army
Development Year 1958
Deployment Year 1962
Retirement Year 1973
Targets land installations
Platform MAZ 543 P TEL(9P117M)
Number manufactured about 7,000 (in Soviet Union)
Design Makeyev SKB-385
Manufacturer Votkinsk MZ

Specification / Performance
Length 11.2m(depending on warhead type)
Body Diameter 88.5cm
Wing/Fin span 1.8m
Launch Weight 5,862-5,950kg
Range 50-300km
Accuracy 610m CEP

Subsystems
Propulsion single-stage liquid-fuel rocket motor
Engine Isayev KBKhM 9D21@rocket engine
Payload 1,016kg
Warhead 200, 300, 500kT nuclear warhead, HE, chemical, submunition warhead (for export)
Guidance inertial

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Scud Mod B/C/ER N.Korea name
Hwasong 5/6(Mars 5/6)



Basic Data
Mission SRBM
Developed by North Korea
Deployed by Cuba, Egypt, Iran, Iraq, Libya, North Korea, Pakistan, Pelu, Syria, Vietnam, Zaire
Service North Korean Air Force
Development Year 1984
Deployment Year 1985
Targets South Korea
Platform Modified MAZ-543 TEL or fixed launch sites (under ground?)
Number manufactured 600-1,000, 50-100 missiles per year during the late 1980s and early 1990s
Number deployed 300-500 (South Korea estimates 500 Scuds. USA estimates 120 Scud ModBs and 180 Scud Mod Cs)
Design The 4th Machine industry bureau
Manufacturer The No.26 General Plant

Specification / Performance
Length 11.25m
Body Diameter 884cm
Launch Weight 5,860kg(Scud Mod B), 5,930kg(Scud Mod C)
Range 320-340km, 500km, 600-1,000km(ER)
Altitude about 30km
Accuracy 450m CEP, 700-1,000m CEP

Subsystems
Propulsion Single-stage liquid
Engine Burn-time=60sec
Payload Single warhead 985kg (length of payload section: 2.87m)
Warhead HE, chemical or submunition
Guidance Inertial

المصدر

http://missile.index.ne.jp/cgi/misearch.cgi

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