(a) |
Magnification of sighting channel |
: 2.7X to 12X |
(b) |
Field of view |
: 20° to 4.5° |
(c) |
Range finding limits |
: 400 to 5000 m |
(d) |
Max range finding error |
: 25 m maximum |
(e) |
Stabilization of FOV |
: Independent, 2 axis |
(f) |
Angles of laying stabilized sighting line
| (i) |
In elevation |
| (aa) Depression |
15° |
| (ab) Elevation |
20° |
| (ii) |
In azimuth |
| (aa) Independent |
± 7° to 9° |
| (ab) With turret |
360° |
|
(g) |
Rate of sighting line laying in elevation and azimuth
| (i) |
Minimum rate, maximum |
0.05° /s |
| (ii) |
Maximum rate, minimum |
3° /s |
|
(h) |
Rate of sighting line slew in azimuth |
:16° to 24° /s |
(i) |
Weight |
: 82 kg |
(j) |
Eyepiece setting range diopter |
: 20 ± 4° |
(k) |
Stabilised sighting line drift
| (i) |
Main Mode |
12 mils/min maximum |
| (ii) |
Double Mode |
16 mils/min maximum |
|
(l) |
Range of distance change due to movement |
:± 500m |
(m) |
Wind velocity cross component measurement range |
:0-25 m/sec |
(n) |
Gun trunion tilt measurement range |
:± 15° |
(o) |
Considered charge and air temperature range |
:± 50°C |
(p) |
Considered Pressure range |
: 0.06 – 0.12 mm Hg |
(q) |
Considered gun barrel wear range |
:3.5 mm |
(r) |
No of radiations per minute (Missile) |
:6 Maximum |
(s) |
Preparation time |
:3 minutes |
(t) |
Continuous operations (non combat) |
:6 hrs |