QW-1
Anza MK-II
| ANZA MK-II Specifications | ||
|---|---|---|
| ||
| L Type | 2-stage, low altitude | |
| Length (missile, with booster motor) | 1.447 m | |
| Weight | 16.5 kg | |
| (total launch assembly in firing condition) (missile at launch) | 10.68 kg | |
| Propulsion | solid fuel booster and solid fuel sustainer rocket motor | |
| Guidance | cooled InSb passive infra-red homing seeker | |
| Warhead | HE fragmentation (containing 0.55 Kg HE) with contact and graze fuzing | |
| Average missile cruise speed | 600 m/s | |
| Max missile manoeuvring | 16 g | |
| Self destruction time | 14-18 s | |
| Max effective slant range | 5,000 m | |
| Min effective slant range | 500 m | |
| Max effective altitude | 4000 m | |
| Min effective altitude | 30 m | |
| Weapon reaction time | less than 3.5 s | |
| Time from march to ready | less than 10 s for operation | |
| Battery operation time | more than 50 s | |
|
NEWSLETTER
|
| Join the GlobalSecurity.org mailing list |
|
|
|
