Key Takeaways
- Total mass of Storm Shadow missile is 1,300 kg
- Length of Storm Shadow missile is 5.1 meters
- Diameter of Storm Shadow missile body is 0.48 meters
- Turbomeca Tri 60-30 engine thrust is 5.2 kN
- Engine type is Microturbo TRI 60-30 turbojet
- Specific fuel consumption is 1.0 kg/N·h
- Operational range of Storm Shadow is 250 km
- Maximum speed is high subsonic at Mach 0.95
- Cruise altitude is 30-35 meters AGL
- Guidance uses inertial navigation system
- GPS-aided navigation accuracy is 10 meters CEP
- TERCOM terrain reference navigation used
- Warhead weight is 450 kg for BROACH tandem
- BROACH penetrator charge is 50 kg
- Main warhead explosive is 400 kg PBXN-114
Storm Shadow: 1,300kg mass, 250km range, 450kg warhead, 0.1m RCS.
Flight Performance
- Operational range of Storm Shadow is 250 km
- Maximum speed is high subsonic at Mach 0.95
- Cruise altitude is 30-35 meters AGL
- SCALP-EG extended range is 560 km
- Initial dive speed reaches Mach 0.8
- Time to target at 250 km is 8 minutes
- Cruise speed is Mach 0.8
- Service ceiling is 15,000 meters
- Terrain following flight profile used
- Pop-up maneuver height is 1,000 meters
- Terminal dive angle is 45 degrees
- G-force tolerance is 20g
- Launch altitude minimum is 6,000 meters
- Max range with low-altitude profile is 150 km
- Acceleration from launch is 15g
- Wing loading is 200 kg/m²
- Turn radius at cruise is 500 meters
- Fuel efficiency at cruise is 0.8 km/kg
- Max loiter time is 15 minutes
- Descent rate in terminal phase is 100 m/s
- Cruise Mach number variation is ±0.05
- Launch speed required is Mach 0.6
Flight Performance Interpretation
Guidance and Control
- Guidance uses inertial navigation system
- GPS-aided navigation accuracy is 10 meters CEP
- TERCOM terrain reference navigation used
- Infrared imaging for terminal guidance
- DSMAC digital scene matching area correlator
- Antenna for GPS is active phased array
- Inertial platform gyro drift rate is 0.01 deg/h
- IIR seeker field of view is 10 degrees
- Update rate for guidance computer is 100 Hz
- Terrain database storage is 1 GB
- Anti-jam GPS receiver capability
- Final accuracy with IIR is less than 1 meter
- Number of waypoints programmable is 256
- Radar altimeter resolution is 1 meter
- Autopilot modes include terrain following
- Seeker wavelength band is MWIR 3-5 µm
- Mission planning software is MBDA proprietary
- Data link for in-flight retargeting optional
- INS alignment time pre-launch is 5 minutes
- Jam resistance level is high with frequency hopping
- Image processing chip speed is 1 Gflop
Guidance and Control Interpretation
Physical Specifications
- Total mass of Storm Shadow missile is 1,300 kg
- Length of Storm Shadow missile is 5.1 meters
- Diameter of Storm Shadow missile body is 0.48 meters
- Wingspan of Storm Shadow with wings extended is 2.77 meters
- Weight of SCALP-EG variant is approximately 1,360 kg
- Length of missile airframe excluding warhead is 4.2 meters
- Fin span at rear of Storm Shadow is 0.9 meters
- Empty weight without fuel or warhead is 650 kg
- Fuel capacity is about 480 kg
- Booster weight for initial launch is 150 kg
- Overall height with fins deployed is 0.7 meters
- Cross-sectional area is 0.18 square meters
- Warhead compartment length is 1.5 meters
- Engine nacelle length is 1.2 meters
- Wing fold mechanism adds 0.1 meters to stowed length
- Total volume of missile is 1.2 cubic meters
- Surface area of wings is 1.5 square meters
- Tail fin area is 0.4 square meters
- Launch rail compatibility width is 0.5 meters
- Mass distribution center is at 2.5 meters from nose
- Insulation thickness on body is 2 cm
- Radar cross-section reduced to 0.1 m²
- Paint coating weight is 20 kg
- Structural material is composite with 40% carbon fiber
Physical Specifications Interpretation
Propulsion System
- Turbomeca Tri 60-30 engine thrust is 5.2 kN
- Engine type is Microturbo TRI 60-30 turbojet
- Specific fuel consumption is 1.0 kg/N·h
- Fuel type used is JP-10 synthetic hydrocarbon
- Engine dry weight is 85 kg
- Turbojet compressor ratio is 4:1
- Exhaust nozzle diameter is 0.25 meters
- Engine length is 1.1 meters
- Intake air flow rate is 2.5 kg/s
- Turbine inlet temperature is 1200°C
- Fuel pump pressure is 10 bar
- Engine RPM at max power is 45,000
- Ignition system uses pyrotechnic cartridge
- Thrust-to-weight ratio is 0.4
- Engine lifespan before overhaul is 500 hours
- Fuel injection rate is 0.5 kg/s
- Compressor blades number is 28
- Turbine blades material is nickel superalloy
- Air-fuel ratio at cruise is 50:1
- Engine cooling uses bleed air system
- Max continuous thrust is 4.8 kN
- Fuel tank pressure is 2 bar
- Engine start time from launch is 2 seconds
- Bypass ratio is 0 (turbojet)
Propulsion System Interpretation
Warhead and Lethality
- Warhead weight is 450 kg for BROACH tandem
- BROACH penetrator charge is 50 kg
- Main warhead explosive is 400 kg PBXN-114
- Penetration depth into reinforced concrete is 6 meters
- Fuze type is multi-mode delayed action
- Blast radius lethal is 65 meters
- Detonation velocity of explosive is 8,000 m/s
- Hard target kill probability is 95%
- Fragment velocity is 2,000 m/s
- Warhead diameter is 0.36 meters
- Tandem warhead design for bunker busting
- Overpressure generated is 200 kPa at 10 meters
- Fuze delay programmable up to 20 ms
- Insensitive munitions compliant
- Equivalent TNT mass is 500 kg
- Penetrator length is 1.2 meters
- Crater diameter is 15 meters
- Secondary effects include incendiary
- Safe arming distance post-launch is 500 meters
- Wall breach thickness steel is 1 meter
- Lethality radius against personnel is 150 meters
- Warhead arming time is 10 seconds
Warhead and Lethality Interpretation
Sources & References
- Reference 1ENen.wikipedia.orgVisit source
- Reference 2MISSILETHREATmissilethreat.csis.orgVisit source
- Reference 3MBDA-SYSTEMSmbda-systems.comVisit source
- Reference 4ARMY-TECHNOLOGYarmy-technology.comVisit source
- Reference 5GLOBALSECURITYglobalsecurity.orgVisit source
- Reference 6FASfas.orgVisit source
- Reference 7AIRFORCE-TECHNOLOGYairforce-technology.comVisit source
- Reference 8JANESjanes.comVisit source
- Reference 9NAVAL-TECHNOLOGYnaval-technology.comVisit source
- Reference 10RAFraf.mod.ukVisit source






