air-launched anti-tank guided missiles (typically launched from helicopters)
air-launched cruise missiles
air-launched anti-ship missiles
anti-radiation missiles
air-launched cruise missiles
air-launched anti-ship missiles
anti-radiation missiles
AGM-28 Hound Dog
| |
AGM-28 in flight (showing the nose-high attitude)
| |
Type
| |
Place of origin
| |
Service history
| |
In service
|
September 13, 1960
|
Production history
| |
Manufacturer
| |
Unit cost
|
$690,073
|
Produced
|
April 1959
|
Specifications
| |
Weight
|
4,603 kilograms (10,147 lb).
|
Length
|
12.95 metres (42 ft 6 in).
|
Height
|
2.84 metres (9 ft 4 in).
|
Diameter
|
710 millimetres (28 in).
|
Warhead
| |
Detonation
mechanism
|
Airburst or Contact
|
Engine
|
Pratt & Whitney J52-P-3 turbojet; 33 kN (7,500 lbf).
|
Wingspan
|
3.71 metres (12 ft 2 in).
|
Operational
range
|
1,263 kilometres (785 mi).
|
Flight ceiling
|
17,100 metres (56,200 ft).
|
Flight altitude
|
61 to 17,069 metres (200 to 56,000 ft).
|
Speed
|
Mach 2.1.
|
Guidance
system
| |
Launch
platform
|
AGM-86
| |
AGM-86A on display at the National Air and Space Museum
| |
Type
|
Air-to-ground strategic cruise missile
|
Place of origin
| |
Service history
| |
In service
|
1982-present[1]
|
Used by
| |
Production history
| |
Designed
|
1974
|
Manufacturer
| |
Unit cost
|
$1 million (AGM-86B)
additional $160,000 conversion cost for AGM-86C;
additional $896,000 conversion cost for AGM-86D[1]
|
Produced
|
1980
|
Number built
|
1,715 (AGM-86B), 239 (AGM-86C), 50 (AGM-86D)[1]
|
Variants
|
AGM-86B (1982), AGM-86C (1991), AGM-86D (2001)
|
Specifications
| |
Weight
|
3,150 pounds (1,430 kg)
|
Length
|
20 ft. 9 in. (6.3 m)
|
Diameter
|
24.5 inches (62 cm)[1]
|
Warhead
|
W80 nuclear warhead (AGM-86B)
Conventional warhead (AGM-86C)
AUP warhead (AGM-86D)
|
Warhead weight
|
2,000 lb class (AGM-86C Block 0)
3,000 lb class (AGM-86C Block 1)
1,200 lb class advanced unitary penetrating warhead (AGM-86D)[1]
|
Engine
|
F107-WR-101 Turbofan Engine
600 lbf (2.7 kN) thrust
|
Wingspan
|
12 feet (3.7 m)
|
Operational
range
|
AGM-86B: 1,500+ mi (2,400+ km)
AGM-86C: classified (nominal 680 miles, 1,100 km)
|
Speed
|
AGM-86B: 550 mph (890 km/h, Mach 0.73)
AGM 86C: classified (nominal high subsonic)
|
Guidance
system
|
AGM-86B: Litton inertial navigation element with terrain contour-matching updates
AGM 86C: Litton INS element integrated with multi-channel onboard GPS
|
Launch
platform
|
Storm Shadow/SCALP EG
| |
Type
|
Long-range, air-to-surface missile
|
Place of origin
| |
Service history
| |
In service
|
2002 – present
|
Used by
|
See Inventory
|
Production history
| |
Manufacturer
| |
Unit cost
|
£790,000[1]
|
Specifications
| |
Weight
|
1,300 kilograms (2,866.0 lb)
|
Length
|
5.1 metres (16.7 ft)
|
Diameter
|
.48 metres (1.6 ft)
|
Warhead
| |
Engine
|
Turbomeca Microturbo TRI 60-30 turbojet, producing 5.4 kN thrust
|
Wingspan
|
2.84 metres (9.3 ft)
|
Operational
range
|
250 km (160 mi)[2]
|
Flight altitude
|
30 metres (98.4 ft)–40 metres (131.2 ft)
|
Speed
|
1,000 km/h Mach 0.8
|
Guidance
system
| |
Launch
platform
|
Eurofighter Typhoon (from 2015)
|
Ra'ad (Hatf VIII)
| |
Type
|
Air-launched cruise missile (ALCM)
|
Place of origin
| |
Service history
| |
In service
|
December 2007 – Present
|
Used by
| |
Production history
| |
Manufacturer
| |
Unit cost
|
Unknown
|
Specifications
| |
Weight
|
1,100 kg
|
Length
|
4.85 m
|
Warhead
|
450 kg HE or nuclear 10 to 35 kt[1]
|
Engine
| |
Operational
range
|
350 km
|
Speed
| |
Guidance
system
| |
Launch
platform
|
ASMP
| |
Type
|
medium-range air to surface nuclear missile
|
Place of origin
|
France
|
Service history
| |
In service
|
1986
|
Production history
| |
Manufacturer
|
Aérospatiale
|
Specifications
| |
Weight
| |
Length
| |
Diameter
| |
Warhead
| |
Engine
|
liquid-fuel ramjet
|
Operational
range
| |
Speed
| |
Launch
platform
|
TAURUS KEPD 350
| |
Type
|
Long-range air-to-surface missile
|
Service history
| |
In service
|
2005
|
Production history
| |
Manufacturer
|
TAURUS Systems GmbH
|
Unit cost
|
950,000 EUR
|
Specifications
| |
Weight
|
1,400 kg
|
Length
|
5.1 m
|
Diameter
|
1.08 m
|
Warhead
| |
Engine
|
Williams P8300-15 Turbofan
|
Wingspan
|
2.064 m
|
Operational
range
|
over 500 km[2]
|
Flight altitude
|
30–40 m
|
Speed
|
Mach 0.80~0.95
|
Guidance
system
|
IBN (Image Based Navigation), INS (Inertial Navigation System), TRN (Terrain Referenced Navigation) and MIL-GPS (Global Positioning System)
|
Launch
platform
|
AGM-129 Advanced Cruise Missile
| |
Type
| |
Service history
| |
In service
|
June 1990 - 2012
|
Used by
|
US Air Force (Decommissioned)
|
Production history
| |
Manufacturer
|
General Dynamics (initially)
|
Produced
|
July 1985
|
Specifications
| |
Weight
|
3,500 lb (1,334 kg)
|
Length
|
20 ft 10 in (6.35 m)
|
Diameter
|
2 ft 5 in (705 mm)
|
Warhead
| |
Engine
| |
Wingspan
|
10 ft 2 in (3.1 m)
|
Operational
range
|
2,000 nautical miles (3,704 km)
|
Speed
|
500 mph (800 km/h)
|
Guidance
system
| |
Launch
platform
|
AGM-158 Joint Air-to-Surface Standoff Missile
| |
Type
|
Air-to-surface cruise missile
|
Place of origin
| |
Service history
| |
In service
|
2009–present
|
Used by
| |
Production history
| |
Manufacturer
| |
Unit cost
|
US$1.327m(JASSM-ER FY13)[1]
|
Produced
|
1998–present
|
Specifications
| |
Weight
|
1021kg (2250lb)
|
Length
|
4.72m (14ft)
|
Warhead
|
450 kg (1000 lb) WDU-42/B penetrator
|
Engine
|
Teledyne CAE J402-CA-100 turbojet
3.0kN (680lb)
|
Wingspan
|
2.4 m (7 ft 11 in)
|
Operational
range
|
370+km (230mi)[JASSM]
1000+km (620mi)[JASSM-ER]
|
Guidance
system
| |
Launch
platform
|
Rafael Popeye
| |
The "Popeye" standoff missile
| |
Type
| |
Place of origin
| |
Service history
| |
In service
|
1985 – present
|
Used by
| |
Production history
| |
Designer
| |
Manufacturer
|
Rafael Advanced Defense Systems
|
Specifications
| |
Weight
|
1,360 kg (3,000 lb)
|
Length
|
4.82 m (15 ft 10 in)
|
Diameter
|
533 mm (21 in)
|
Warhead
|
340 kg (750 lb) blast fragmentation or 360 kg (800 lb) I-800 penetrating
|
Engine
|
Single-stage Solid-fuel rocket
|
Wingspan
|
198 cm (78 in)
|
Operational
range
|
78 km (48 miles)
|
Guidance
system
|
Inertial plus IIR or TV
|
Launch
platform
|
Fixed-wing aircraft, Dolphin class submarine (Popeye Turbo SLCM)
|
'K' Missile family
| |
Type
| |
Place of origin
| |
Service history
| |
In service
|
In production (k-15)[1]
2017 (k-4)[2]
|
Used by
| |
Production history
| |
Manufacturer
| |
Produced
|
K-15 In production
|
Specifications
| |
Weight
|
17 tonnes (K-4)[5]
2 tonnes (Air-launched)
|
Length
|
10m (K-15, K-4 present)
12m (K-4 future variant)
|
Width
|
0.74m (K-15)
1.3m (K-4)
|
Maximum firing range
|
5,000 km (unnamed Longer legged variant of K-4)[2]
|
Warhead
|
K-15:1 tonne,
K-4:1-2.5 tonnes,[5]
K-5:1 tonne
500 kg (Air-Launched Version)
|
Blast yield
|
K-4: 200-250 kilotons[5]
|
Operational
range
|
3,500 km
|
Maximum depth
|
over 50m (tested)
|
Speed
| |
Launch
platform
|
The K family of missiles is a series
TYPE
|
RANGE
|
Weight
|
Warhead
|
length
|
Status
|
750 km-1,500 km
|
1 tonne
|
10 m
| |||
3,500 km
|
20 tonnes[5]
|
2.5 tonnes[5]
|
10 m
| ||
5,000 km[2]
|
17 tonnes
|
1 tonne[2]
|
12 m
|
Under development
| |
Air Launched[2]
|
200 km
|
2 tonnes
|
500 kg
|
4 m
|
Hypersonic missile project called ‘Air launched article’. It is designated to fit with Sukhoi Su-30-MKI. First prototype will be ready by 2012.
|
K-5
|
6,000 km[12]
|
Unspecified
|
1 tonne
|
Unspecified
|
SOM Cruise Missile
| |
SOM cruise missile mockup exhibited during MSPO 2014 at Kielce, Poland.
| |
Type
| |
Place of origin
| |
Service history
| |
In service
|
Since 2012
|
Production history
| |
Manufacturer
| |
Specifications
| |
Weight
|
600 kilograms (1,323 lb)
|
Length
|
3,657 millimetres (12.0 ft)[1]
|
Warhead
|
230 kilograms (507 lb)
SOM-A: High Explosive
SOM-B1: High Explosive
SOM-B2: Dual-stage penetrator
|
Engine
|
Microturbo TRI 40
2.5-3.3 kN
|
Wingspan
|
2,600 millimetres (8.53 ft)
|
Operational
range
|
300 kilometres (162 nmi) (tested range)
500 kilometres (270 nmi) (claimed range)
|
Flight altitude
| |
Speed
|
623 knots (0.94 Mach )
|
Guidance
system
|
Image Based Navigation
|
Accuracy
|
5 metres (16 ft) CEP
|
Launch
platform
|
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