ALAS
175 mm guided missile ALAS
A turbojet-sustained guided missile launched from a container by a solid propellant booster, using INS/GNSS mid-course guidance and TV CCD or IIR terminal guidance with contrast/correlation auto tracking, and carrying a tandem-charge HEAT warhead with additional blast fragmentation; it is controlled over a single-mode optical fibre link or an optional two-way C-band radio link.
يُكتب أيضاً: 175
تكبير 175 mm guided missile ALAS
المواصفات
| Total body length | 2.723 m |
|---|---|
| Body diameter (caliber) | 0.175 m |
| Wingspan | 1.638 m |
| Launching weight | 73.10 kg |
| Weight in flight | 59.3 kg |
| Sustainer propulsion (type) | TMM-040/RC turbojet engine |
| Turbojet engine max. net thrust | 400 N |
| Booster propulsion (type) | solid propellant booster engine |
| Cruising speed | 120-150 m/s |
| Max. flight altitude above sea level | 2000 m |
| Max. effective range | 25 km |
| Min. effective range | 4 km |
| Max. axial load | 10 g |
| Max. operational load limit | 4 g |
| Mid-course guidance | INS/GNSS |
| Terminal guidance | TV CCD/IIR |
| Auto tracking | contrast/correlation tracking algorithm |
| Warhead | tandem-charge HEAT with additional blast fragmentation |
| Safety and arming | safety arming mechanism with proximity fuse |
| Turbojet Mach number range | 0 - 0.8 |
| Specific fuel consumption | 1.40 kg/daNh |
| Total engine life | 10 h |
| Booster total impulse | 10720 Ns |
| Booster maximum thrust | 6000 N at 15 °C |
| Communication | single-mode optical fibre, signal loss less than 15 dB |
| Radio link | C-band, two-way, data rate up to 100 kbps |
| Homing head | TV CCD or IR sensor on gyro stabilized gimbal |
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