Specifications | |||
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DIA |
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NATO |
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Bilateral |
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Service |
RT-25 |
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OKB/Industry |
8K97 |
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Design Bureau |
OKB-1/Mashinosteroeniya |
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Approved |
4/4/1961 |
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Years of R&D |
1961-1966 |
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Engineering and Testing |
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First Flight Test |
No flight tests conducted |
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IOC |
Not operational |
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Deployment Date |
Not deployed |
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Type of Warhead |
Single |
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Warheads |
1 |
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Yield (Mt) |
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Payload (t) |
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Total length (m) |
15-16 |
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Total length w/o warhead (m) |
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Missile Diameter (m) |
2-1.84 |
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Launch Weight (t) |
40-42 |
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Range (km) |
4000-5000 |
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CEP (m) |
? |
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Number of Stages |
2 |
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Canister length (m) |
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Canister length w/o front meters (m) |
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Canister diameter (m) |
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Booster guidance system |
Inertial autonomous |
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1st stage |
2nd stage |
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Length (m) |
8.7 |
3.83 |
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Body diameter (m) |
2.0-1.84 |
1.01 |
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Fueled weight (t) |
34.5 |
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Dry weight (t) |
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Solid Motor Designation |
15D23 |
15D25 |
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Design Bureau |
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Years R & D |
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Propellants |
Solid motor |
Solid motor |
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Fuel |
N/A |
N/A |
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Oxidizer |
N/A |
N/A |
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Burning time (sec.) |
75 |
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Thrust Sea Level/Vacuum (Tonnes) |
91 |
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Specific Impulse Sea Level/Vacuum (sec.) |
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Basing Mode mobile, silo concept |
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Hardness |
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Launching Technique Hot launch |
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Deployed boosters 0 |
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Test Boosters |
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Warheads Deployed 0 |
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Deployment Sites |
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Training Launchers |
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Space Booster Variant N/A |