 |
SS-X-10 'Scrag' Universal Ballistic Missile System |
|
|
|
SS-X-10 'Scrag' Universal Ballistic Missile System |
|
|
SS-X-10 'Scrag' Ballistic Missile |
||
| Designer: | V. N. Chelomei | |
|
Manufacturer: |
OKB-52 |
|
|
Role: |
Universal Rocket System |
|
| Soviet Designation: | GR-1 and UR-200 | |
|
Year Adopted: |
Never entered service |
|
|
Operational Status: |
Russia - Experimental only. Was cancelled in 1964 before deployment. |
|
|
Warheads: |
A single 5 or 15 Megaton warhead |
|
|
Engine: |
RD-204 (1st stage) |
|
| Fuel: | Liquid Oxygen, Kerosene, Nitrogen Tetroxide | |
|
Length: |
34.65 meters |
(113.7 feet) |
|
Width: |
10 meters |
(32.8 feet) |
|
Weight at Launch: |
138 metric tons |
(135.8 Tons) |
|
Launch Type: |
Hot Launched, Soft Site Based |
|
|
Range: |
1400 kilometers |
(869.9 miles) |
| CEP (Circular Probability of Error): | 1800 to 5500 meters | (1.1 to 3.4 miles) |