UNITED24 - Make a charitable donation in support of Ukraine!

Weapons of Mass Destruction (WMD)


RT-1 ICBM


Specifications
DIA      
NATO      
Bilateral      
Service   RT-1 RT-1-63
OKB/Industry   (8k95-63) (8K95-1963)
Design Bureau   OKB-1, Acad. S. P. Korolev OKB-1, Acad. S. P. Korolev
Approved   11-20-59 11-20-59
Years of R&D   1958/59 -1962 1962,-1963/1964
Engineering and Testing   1960 -1963 1962 -1963
First Flight Test   04/28/1962 failure 3/18/1963 success cancelled 9-11/ /1965, 2 failures one success cancelled
IOC   N/A N/A
Deployment Date   N/A N/A
Type of Warhead   Single Single
Warheads   1 1
Yield (Mt)   0.5 -1.0 0.6 -1.0
Payload (t)   0.5 - 0.8 0.8
Total length (m)   18.0 18.3
Total length w/o warhead (m)      
Missile Diameter (m)   2.0 2.0
Launch Weight (t)   35.5-36.0 (34) 34 -35.5
Fuel Weight (t)      
Range (km)   1,850-2,000 2,400-2,500
CEP (m) (Russian Sources)      
CEP (m) Western Sources)      


Number of Stages   3 3
Canister length (m)      
Canister length w/o
front meters (m)		      
Canister diameter (m)      
Booster guidance system   Inertial Inertial


    1st stage   2nd stage 3rd Stage
Length (m)   4.6-4.8   3.9-4.0 2.8
Body diameter (m)   1.6 x 4   1.5 x 4 1.4
Fueled weight (t)          
Dry weight (t)          
Engine Designation          
Configuration          
Design Bureau          
Years of R & D          
Propellants   Solid Propellant   Solid Propellant Solid Propellant
Fuel   Solid Propellant   Solid Propellant Solid Propellant
Oxidizer   Solid Propellant   Solid Propellant Solid Propellant
Burning time (sec.)   30 -32   17.5 -30 30 - 42
Thrust Sea Level/Vacuum (Tonnes)   100   51 25
Specific Impulse Sea Level/Vacuum (sec.)   204   223  


Basing Mode   N/A  
Hardness      
Launching Technique   Hot Launch  
Deployed boosters   0  
Test Boosters      
Warheads Deployed   0  
Deployment Sites   0  
Training Launchers   0  
Space Booster Variant   N/A  



NEWSLETTER
Join the GlobalSecurity.org mailing list