Initial Operational Capability (IOC):
Total Production: ?
Also Known As: Light Weight Self Propelled Howitzer
Origin: Singapore
Corporations: ST Engineering
Parent System: LWSPH
Initial Operational Capability (IOC):
Total Production: ?
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Description: The LWSPH (Light Weight Self-Propelled Howitzer) is an air-transportable by both aircraft and helicopter, 155mm 39-caliber, self-propelled howitzer. It is mounted on a 4x4 chassis that lacks of external armor to protect the crew helping to keep the overall LWSPH weight around 7 tons.

The LWSPH maximum range with unassisted projectiles is 19km, while that figure increases dramatically to 30 kilometers with rocket assisted projectiles.

The LWSPH was certified for air-transportation by C-130 aircraft, CH-53 and CH-47 helicopters.

LWSPH Specifications

Crew: 4
Wheel Drive: 4x4
Height: 2.60 meter
Length: 10 meter
Main Gun Caliber: 155 millimeter
Width: 2.50 meter
Main Gun Max Range: 19,000 meter (11.8 mile)
Max Range: 600 kilometer
Max Range firing RAP: 30,000 meter
Power: 170 shp (127 kW)
Max Rate of Fire: 6 roundperminute
Sustained Rate of Fire: 2 roundperminute
Top Speed: 22.3 mps (80 kph)
Combat Weight: 7,000 kilogram
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

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