|
Entered service |
? |
|
Crew |
5 men |
|
Dimensions and weight |
|
Weight |
~ 22 t |
|
Length (gun forward) |
? |
|
Hull length |
? |
|
Width |
? |
|
Height |
? |
|
Armament |
|
Main gun |
155-mm gun-howitzer |
|
Barrel length |
52 calibers |
|
Machine guns |
- |
|
Projectile weight |
? |
|
Maximum firing range |
30 - 41 km |
|
Maximum rate of fire |
4 - 9 rpm |
|
Elevation range |
? to + 70 degrees |
|
Traverse range |
50 degrees |
|
Ammunition load |
|
Main gun |
32 rounds |
|
Machine guns |
- |
|
Mobility |
|
Engine |
MAN 2866 LF 24 diesel |
|
Engine power |
360 hp |
|
Maximum road speed |
? |
|
Range |
? |
|
Maneuverability |
|
Gradient |
? |
|
Side slope |
? |
|
Vertical step |
? |
|
Trench |
? |
|
Fording |
? |
|
The ATROM
self-propelled artillery system is a Romanian variant of the Israeli
ATMOS 2000. The ATROM was first
revealed in 2003.
The ATROM is
fitted with the Soltam 155-mm / L52 gun-howitzer. The same weapon is
used on the ATMOS 2000. This gun-howitzer id fitted with a load
assisting system. Maximum range of fire is 41 km with rocket
assisted projectile and 30 km with standard HE projectile. The ATROM
is compatible with all standard 155-mm NATO ammunition. Maximum rate
of fire is between 4 and 9 rounds per minute. The ATROM is capable
of firing 3 rounds in 20 seconds.
Fire
computerized control system of the ATROM is coupled to an internal
navigation system. Target information is received from forward
observers.
Vehicle has
a crew of five. Armored cab provides protection from small arms fire
and artillery shell splinters.
The ATROM
uses locally developed ROMAN 26.360 DFAEG 6x6 truck chassis. Vehicle
is powered by a MAN 28866 LF 24 diesel engine, developing 360 hp.
The ATROM is fitted with auxiliary power unit, which powers all
systems when the main engine is shut down. The ATROM can be
airlifted with a
C-130 Hercules medium
transport aircraft.
|
Video of the ATROM
self-propelled artillery system |
|
|