GITNUXREPORT 2026

Storm Shadow Missile Statistics

Storm Shadow: 1,300kg mass, 250km range, 450kg warhead, 0.1m RCS.

Sarah Mitchell

Sarah Mitchell

Senior Researcher specializing in consumer behavior and market trends.

First published: Feb 24, 2026

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Key Statistics

Statistic 1

Operational range of Storm Shadow is 250 km

Statistic 2

Maximum speed is high subsonic at Mach 0.95

Statistic 3

Cruise altitude is 30-35 meters AGL

Statistic 4

SCALP-EG extended range is 560 km

Statistic 5

Initial dive speed reaches Mach 0.8

Statistic 6

Time to target at 250 km is 8 minutes

Statistic 7

Cruise speed is Mach 0.8

Statistic 8

Service ceiling is 15,000 meters

Statistic 9

Terrain following flight profile used

Statistic 10

Pop-up maneuver height is 1,000 meters

Statistic 11

Terminal dive angle is 45 degrees

Statistic 12

G-force tolerance is 20g

Statistic 13

Launch altitude minimum is 6,000 meters

Statistic 14

Max range with low-altitude profile is 150 km

Statistic 15

Acceleration from launch is 15g

Statistic 16

Wing loading is 200 kg/m²

Statistic 17

Turn radius at cruise is 500 meters

Statistic 18

Fuel efficiency at cruise is 0.8 km/kg

Statistic 19

Max loiter time is 15 minutes

Statistic 20

Descent rate in terminal phase is 100 m/s

Statistic 21

Cruise Mach number variation is ±0.05

Statistic 22

Launch speed required is Mach 0.6

Statistic 23

Guidance uses inertial navigation system

Statistic 24

GPS-aided navigation accuracy is 10 meters CEP

Statistic 25

TERCOM terrain reference navigation used

Statistic 26

Infrared imaging for terminal guidance

Statistic 27

DSMAC digital scene matching area correlator

Statistic 28

Antenna for GPS is active phased array

Statistic 29

Inertial platform gyro drift rate is 0.01 deg/h

Statistic 30

IIR seeker field of view is 10 degrees

Statistic 31

Update rate for guidance computer is 100 Hz

Statistic 32

Terrain database storage is 1 GB

Statistic 33

Anti-jam GPS receiver capability

Statistic 34

Final accuracy with IIR is less than 1 meter

Statistic 35

Number of waypoints programmable is 256

Statistic 36

Radar altimeter resolution is 1 meter

Statistic 37

Autopilot modes include terrain following

Statistic 38

Seeker wavelength band is MWIR 3-5 µm

Statistic 39

Mission planning software is MBDA proprietary

Statistic 40

Data link for in-flight retargeting optional

Statistic 41

INS alignment time pre-launch is 5 minutes

Statistic 42

Jam resistance level is high with frequency hopping

Statistic 43

Image processing chip speed is 1 Gflop

Statistic 44

Total mass of Storm Shadow missile is 1,300 kg

Statistic 45

Length of Storm Shadow missile is 5.1 meters

Statistic 46

Diameter of Storm Shadow missile body is 0.48 meters

Statistic 47

Wingspan of Storm Shadow with wings extended is 2.77 meters

Statistic 48

Weight of SCALP-EG variant is approximately 1,360 kg

Statistic 49

Length of missile airframe excluding warhead is 4.2 meters

Statistic 50

Fin span at rear of Storm Shadow is 0.9 meters

Statistic 51

Empty weight without fuel or warhead is 650 kg

Statistic 52

Fuel capacity is about 480 kg

Statistic 53

Booster weight for initial launch is 150 kg

Statistic 54

Overall height with fins deployed is 0.7 meters

Statistic 55

Cross-sectional area is 0.18 square meters

Statistic 56

Warhead compartment length is 1.5 meters

Statistic 57

Engine nacelle length is 1.2 meters

Statistic 58

Wing fold mechanism adds 0.1 meters to stowed length

Statistic 59

Total volume of missile is 1.2 cubic meters

Statistic 60

Surface area of wings is 1.5 square meters

Statistic 61

Tail fin area is 0.4 square meters

Statistic 62

Launch rail compatibility width is 0.5 meters

Statistic 63

Mass distribution center is at 2.5 meters from nose

Statistic 64

Insulation thickness on body is 2 cm

Statistic 65

Radar cross-section reduced to 0.1 m²

Statistic 66

Paint coating weight is 20 kg

Statistic 67

Structural material is composite with 40% carbon fiber

Statistic 68

Turbomeca Tri 60-30 engine thrust is 5.2 kN

Statistic 69

Engine type is Microturbo TRI 60-30 turbojet

Statistic 70

Specific fuel consumption is 1.0 kg/N·h

Statistic 71

Fuel type used is JP-10 synthetic hydrocarbon

Statistic 72

Engine dry weight is 85 kg

Statistic 73

Turbojet compressor ratio is 4:1

Statistic 74

Exhaust nozzle diameter is 0.25 meters

Statistic 75

Engine length is 1.1 meters

Statistic 76

Intake air flow rate is 2.5 kg/s

Statistic 77

Turbine inlet temperature is 1200°C

Statistic 78

Fuel pump pressure is 10 bar

Statistic 79

Engine RPM at max power is 45,000

Statistic 80

Ignition system uses pyrotechnic cartridge

Statistic 81

Thrust-to-weight ratio is 0.4

Statistic 82

Engine lifespan before overhaul is 500 hours

Statistic 83

Fuel injection rate is 0.5 kg/s

Statistic 84

Compressor blades number is 28

Statistic 85

Turbine blades material is nickel superalloy

Statistic 86

Air-fuel ratio at cruise is 50:1

Statistic 87

Engine cooling uses bleed air system

Statistic 88

Max continuous thrust is 4.8 kN

Statistic 89

Fuel tank pressure is 2 bar

Statistic 90

Engine start time from launch is 2 seconds

Statistic 91

Bypass ratio is 0 (turbojet)

Statistic 92

Warhead weight is 450 kg for BROACH tandem

Statistic 93

BROACH penetrator charge is 50 kg

Statistic 94

Main warhead explosive is 400 kg PBXN-114

Statistic 95

Penetration depth into reinforced concrete is 6 meters

Statistic 96

Fuze type is multi-mode delayed action

Statistic 97

Blast radius lethal is 65 meters

Statistic 98

Detonation velocity of explosive is 8,000 m/s

Statistic 99

Hard target kill probability is 95%

Statistic 100

Fragment velocity is 2,000 m/s

Statistic 101

Warhead diameter is 0.36 meters

Statistic 102

Tandem warhead design for bunker busting

Statistic 103

Overpressure generated is 200 kPa at 10 meters

Statistic 104

Fuze delay programmable up to 20 ms

Statistic 105

Insensitive munitions compliant

Statistic 106

Equivalent TNT mass is 500 kg

Statistic 107

Penetrator length is 1.2 meters

Statistic 108

Crater diameter is 15 meters

Statistic 109

Secondary effects include incendiary

Statistic 110

Safe arming distance post-launch is 500 meters

Statistic 111

Wall breach thickness steel is 1 meter

Statistic 112

Lethality radius against personnel is 150 meters

Statistic 113

Warhead arming time is 10 seconds

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Ever wanted to know what makes the Storm Shadow missile a fearsome and intricate weapon? This blog post breaks down its critical statistics, from its 1,300 kg total mass and 5.1-meter length to its powerful Microturbo TRI 60-30 turbojet engine, 250 km operational range, advanced GPS and terrain-reference guidance systems, and a 450 kg warhead that delivers a 95% hard target kill probability, all explained through clear, accessible details.

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

The Storm Shadow missile is a sharp, long-range tool that zips at high subsonic speeds (up to 0.95 Mach) from low altitudes—just 30 to 35 meters above the ground—uses terrain-following to hug the terrain, pops up to 1,000 meters when needed, dives at 45 degrees at 100 meters per second, accelerates hard (15g from launch, 20g max), can reach 560 km away in under 8 minutes with low-altitude fuel efficiency (0.8 km per kg), loiters for up to 15 minutes, keeps its speed steady within ±0.05 Mach, launches from at least 6,000 meters, turns tightly (500-meter radius at cruise), and has a 200 kg/m² wing loading, making it both precise and adaptable mid-flight.

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

The Storm Shadow missile is a precision prodigy, mixing inertial navigation (with a rock-steady gyro that drifts just 0.01 degrees per hour) with GPS (active phased array, anti-jam, and terrain/ scene matching to sharpen accuracy from 10 meters CEP to under 1 meter at the end, thanks to its infrared wizardry), zipping through 256 waypoints, hugging terrain at meter-level precision, hopping frequencies to outsmart jammers, updating its target 100 times a second, and even letting you tweak its course mid-flight (if you want), all powered by a 1Gflop processor and MBDA’s secret mission-planning software.

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

The Storm Shadow, a missile that blends military precision with meticulous engineering, weighs up to 1,360 kg (1,300 kg for the base model), stretches 5.1 meters long (4.2 meters without a warhead, with a 0.1-meter shorter stowed length due to wing fold), has a 0.48-meter-wide body, a 2.77-meter extended wingspan, and stands 0.7 meters tall with fins down; its 650 kg empty weight (without fuel or warhead) holds 480 kg of fuel and 150 kg of booster, boasting a 0.18-square-meter cross-sectional area; crafted from 40% carbon fiber composites—coated with 20 kg of paint, insulated with 2 cm of material, and shaped to a radar cross-section of just 0.1 square meters—it features a 1.5-meter warhead compartment, a 1.2-meter engine nacelle, 1.5 square meters of wing surface area, 0.4 square meters of tail fin area, and fits into 1.2 cubic meters, all compatible with 0.5-meter-wide launch rails, with its mass balanced neatly 2.5 meters from the nose.

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

The Storm Shadow's Microturbo TRI 60-30 turbojet, a compact yet purposeful engine, churns out 5.2 kN of peak thrust (4.8 kN continuously) in just 2 seconds, drinks JP-10 synthetic fuel at 1.0 kg per kN per hour, skips the bypass (a pure turbojet), uses nickel superalloy turbine blades, and manages a modest 0.4 thrust-to-weight ratio—but with 28 compressor blades spinning at 45,000 RPM and a 4:1 pressure ratio, it balances raw punch with quiet practicality, making it a key piece of the missile’s precision punch.

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

The Storm Shadow, built for bunker-busting, packs a 450kg warhead—including a 50kg penetrator and 400kg PBXN-114 explosive, with an equivalent TNT mass of 500kg—that bores 6 meters into reinforced concrete or breaks through 1 meter of steel, uses a multi-mode, 20ms programmable fuze to detonate 500 meters after launch and arm 10 seconds post-launch, sprays fragments at 2,000 m/s, leaves a 65m lethal blast radius, generates 200 kPa of overpressure at 10 meters, creates a 15m crater, and has a 95% hard-target kill probability, plus incendiary secondary effects—clearly designed to handle fortified targets with precision and raw power.