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Weapons of Mass Destruction (WMD)


UR-100N / SS-19 STILLETO


Specifications
  Mod-1 Mod-2 Mod-3
DIA SS-19 SS-19 SS-19
NATO Stiletto Stiletto Stiletto
Bilateral RS-18A RS-18A UTTKh RS-18B
Service UR-100N UR-100N UR-100NU
OKB/Industry 15A30 15A30 15A35
Design Bureau OKB-52, KB Salyut,
Acad. V. N. Chelomey
OKB-52, KB Salyut,
Acad. V. N. Chelomey
OKB-52, KB Salyut,
Acad. V. N. Chelomey
Approved 8/19/1970 8/19/1970 8/16/1976
Years of R&D 1964-73 1964-1973  
Engineering and
Testing
1973-75 1973-75 1977-79
First Flight Test 9/15/1972 failure & 12/28/1973 success 4/9/1973 10/26/1977
IOC 4/26/1975 1975 1979
Deployment Date 12/301975 12/30/1975 11/5/1979
Type of Warhead MIRV Single MIRV
Warheads 6 1 6
Yield per Warhead (Mt) 0.5 0.55 0.750 2.5 - 5.0 0.5-0.75
Payload (t) 4.350 4.350 4.350
Total length (m) 24.0 24.0 24.3
Total length w/o
Warhead (m)
21.1 21.1 21.1
Missile Diameter (m) 2.50 2.50 2.50
Launch Weight (t) 103 - 105.6 105.6 103.4 - 105.6
Fuel Weight (t) 93.1 93.1 93.1
Range (km) 9,650 10,000 10,000
CEP (m)
(Russian Sources)
? ? 920
CEP (m)
(Western Sources)
350-550 250-400 220-380


Number of Stages 2
Canister length (m) 19.4
Canister length w/o
front meters (m)
 
Canister diameter (m) 2.9
Booster guidance system Inertial


  1st stage 2nd stage 3rd. Stage
Length (m) 17.2 2.8  
Body diameter (m) 2.5 2.5 2.5
Fueled weight (t) 86.3 86.3  
Dry weight (t)      
Engine Designation RD-0233 / RD-0234 RD-0235 (14/15D113) N/A
Vernier Engine Designation N/A RD-0236 (15D114) N/A
Bus Engine Designation Third Stage N/A N/A RD-0237
Design Bureau Main Engines OKB-154, Acad. S. A. Kosberg OKB-154, Acad. S. A. Kosberg N/A
Design Bureau Vernier Engine N/A OKB-154, Acad. S. A. Kosberg N/A
Design Bureau Bus Engine Third Stage N/A N/A OKB-154, Acad. S. A. Kosberg
Configuration Cluster of four engines One engine N/A
Configuration Vernier Engine N/A Four vernier chambers N/A
Configuration Bus engine Third Stage N/A N/A Four chambers
Years of R & D 1969 1974 1969 - 1974 N/A
Years of R & D Vernier Engine N/A 1969 - 1974 N/A
Years of R & D Bus Engine Third Stage N/A N/A 1969 - 1974
Propellants Liquid Liquid Liquid
Fuel UHMH UDMH UDMH
Oxidizer Nitrogen Tetroxide Nitrogen Tetroxide Nitrogen Tetroxide
Burning time (sec.)      
Main Engine Thrust Sea Level/Vacuum (Tonnes) 46.961/52.958 - 53.1 24.5 Vacuum N/A
Verniers Thrust Sea Level/Vacuum (Tonnes) N/A 1.6 Vacuum N/A
Third Stage Bus Engine Thrust Vacuum (Tonnes) N/A N/A 0.5 Vacuum
Total Thrust Sea Level/Vacuum (Tonnes) 187.8442/207.8319 30.9 Vacuum 2.0 Vacuum
Main Engine Specific Impulse Sea Level/ Vacuum (sec.) 291 / 310 320 Vacuum N/A
Vernier Engine Specific Impulse Sea Level/Vacuum (sec.) N/A 293 Vacuum N/A
Bus Third Stage Engine Specific Impulse Vacuum (sec.) N/A N/A ?


Basing Mode Silo
Hardness  
Launching Technique Hot
Deployed Boosters  
Test Boosters  
Warheads Deployed  
Training Launchers  
Space Booster Variant Yes SL-X- ? , Rockot




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Page last modified: 29-05-2019 19:06:25 ZULU