|
Oka missile system |
| Year of adoption |
1983 |
| Developer |
Engineering Bureau of the city of Kolomna |
| Manufacturer |
Vokkinskiy Machine-building plant |
| Variants |
Rocket 9M714B - SS-23 SPIDER-A
Rocket 9M714F - SS-23 SPIDER-B
Rocket 9M714K - SS-23 SPIDER-C |
|
Rocket 9M714K / 9M714B |
| Number of steps, PCs |
1 |
| Maximum diameter, m |
0970 |
| Length, M |
7,516 in/7,315 |
| Starting weight of the rocket, kg |
4630 in/4400 |
| Maximum firing range, km |
400 in/300 |
| Firing Range min, km |
50 |
| Maximum trajectory height, km |
120 |
| Accuracy of shooting (Kwo), km |
0.35 |
| Weight of the combat unit, KG |
715 in/375 |
|
9P71 Launch unit/transport-charging machine 9t 230 |
| Wheel Formula |
8x8 |
| Total weight, kg |
29100 in/29985 |
| Length, M |
11,760 in/11,800 |
| width, M |
3,130 in/3,000 |
| Height, M |
3,000 |
| Speed on land, km/h |
65 |
| Speed afloat, km/h |
8-10 |
| Power Reserve, km |
700 |
| Engine power of the Utd-25, L. s |
400 |
