RT-15 / RT-2P
SS-14 SCAMP / SCAPEGOAT
| Specifications | ||
|---|---|---|
| DIA | SS-X-14 (SS-14) | |
| NATO* | Scamp/ Scapegoat | |
| Bilateral | ||
| Service | RT-15 | |
| OKB/Industry | 8K96 | |
| Design Bureau | KB Arsenal (Tyurin-OKB) TsKB-7 | |
| Approved | 4/4/1961 | |
| Years of R&D | 1958-63 | |
| Engineering and Testing | 1966-1968 | |
| First Flight Test | 9/__/1965 | |
| IOC | Not operational 3/__/1970 | |
| Deployment Date | Not deployed 3/__/1970 | |
| Type of Warhead | Single | |
| Warheads | 1 | |
| Yield (Mt) | 1 | |
| Payload (t) | 0.535 | |
| Total length (m) | 11.93 | |
| Total length w/o warhead (m) | 11.74 | |
| Missile Diameter (m) | 1.49 | |
| Launch Weight (t) | 16 | |
| Range (km) | 2500-2,950 | |
| CEP (m) (Russian Sources) | 0.9 km | |
| CEP (m) (Western* Sources) | 600-2000 | |
| Number of Stages | 2 | |
| Canister length (m) | 12,7 | |
| Canister length w/o front meters (m) | ||
| Canister diameter (m) | 2,1 | |
| Booster guidance system | Inertial autonomous | |
| 1st stage | 2nd stage | |||
| Length (m) | 4.74 | 6.77 | ||
| Body diameter (m) | 1.49 | 1.01 | ||
| Fueled weight (t) | ||||
| Dry weight (t) | ||||
| Solid Motor Designation | 15D27 | 15D2 or 15D92 | ||
| Design Bureau | ||||
| R & D Years | ||||
| Propellants | Solid | Solid | ||
| Fuel | N/A | N/A | ||
| Oxidizer | N/A | N/A | ||
| Burning time (sec.) | 60 | 45 | ||
| Thrust Sea Level/Vacuum (Tonnes) Specific Impulse (sec.) |
42 237/263 |
22 271 |
||
| Basing Mode | Ground Mobile | |
| Hardness | ||
| Launching Technique | Hot | |
| Deployed boosters | 0 | |
| Test Boosters | ||
| Warheads Deployed | 0 | |
| Deployment Sites | ||
| Training Launchers | ||
| Space Booster Variant | N/A |
|
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