SLAM-2
Infobox
SLAM-2
| Statistics | Info |
|---|---|
| First designed by | Fox Corporation |
| First released in | 1746 |
| Manufactured & developed by | Fox Corporation |
| Environment | Space |
| Guidance | Infrared |
| Aspect | Rear |
| Seeker gimbal | Caged |
| ITAS | N/A |
| Relative manoeuvrability | 15 G |
| Flare resistance class | 0 |
| Maximum lock range | 3.2 km |
| Maximum flight range from stationary | 5.2 km |
| Initial mass | 79.4 kg |
| Thrust force | 17,000 N |
| Initial acceleration | 214.11 ms-2 |
| Forwards thrust time | 3.5 seconds |
| Guidance thrust time | 6.0 seconds |
The Space Launched Assault Missile - 2 was a basic rear-aspect infrared combat missile designed by the Fox Corporation for use in space during starship to starship engagements. Developed off of the SLAM-1 with newfound funding, the -2 variant featured an upgraded motor, improved agility from reprogrammed reaction control system thrusters and more guidance thrust time - an all around improvement over the former.