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Weapons of Mass Destruction (WMD)


R-13 / SS-N-4 SARK

Specifications
DIA SS-N-4
NATO Sark
Bilateral  
Service R-13
OKB/Industry 4K50
Design Bureau SKB-385
Approved  
Years of R&D  
Engineering and Testing 1959-1960
First Flight Test 1959
IOC  
Deployment Date 10/13/1961
Launch system D-2/D-3
Submarine Golf & Hotel class
Type of Warhead Single
Warheads 1
Yield (mt) 1
Payload (t) 1.6
Total length (m) 11.8
Total length w/o warhead (m)  
Missile Diameter (m) 1.3
Diameter of Stabilizers (m) 1.9
Launch Weight (t) 13.745
Fuel Weight (t)  
Range (km) 600
CEP (m) (Russian Sources) 4,000
CEP (m) Western Sources) 1,800 - 3,900
Number of Stages 1
Warheads Deployed  
Booster guidance system  
Engine Designation  
Propellants Liquid
Fuel AK-27I
Oxidizer TG-02
Burning time (s)  
Verniers Thrust Sea Level/Vacuum (kn)  
Specific Impulse (s)  
Launching Technique Surfaced



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Page last modified: 24-07-2011 04:48:22 ZULU