Initial Operational Capability (IOC):
Parent System: PGHSLD-500
Initial Operational Capability (IOC): 2018
Maiden Flight: September 2017
Total Production: ?
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Description: The PGHSLD-500 is a precision guided bomb developed by India's DRDO based upon the High Speed Low Drag (HSLD) bomb design. The new 500 kilogram guided bomb was first tested by the Indian Air Force from a Su-30MKI aircraft. The bomb has been designed to engage ground targets such as railways, bridges, industrial facilities, bunkers, runways and other hardened targets. The PGHSLD-500 glide bomb is intended for use by Su-30MKI, Jaguar and Mig-29 fighters for strike missions.
Max Maneuvering Load Factor: 6.50 g
Max Launch Altitude: 5,000 meter (16,404 foot)
Min Launch Altitude: 150 meter
Max Launch Airspeed: 900 kph
Weight: 500 kilogram (1,102 pound)
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)
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on 8 Sep 2017
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