Air-launched cruise missile

air-launched anti-tank guided missiles (typically launched from helicopters)
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	Cruise Missile
Place of origin	United States
Service history
In service	September 13, 1960
Production history
Manufacturer	North American Aviation
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	790 kilograms (1,742 lb) W28 Class D bomb.
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	Inertial with star-tracker correction.
Launch platform	B-52 Stratofortress.

AGM-86
AGM-86A on display at the National Air and Space Museum
Type	Air-to-ground strategic cruise missile
Place of origin	United States
Service history
In service	1982-present[1]
Used by	United States Air Force
Production history
Designed	1974
Manufacturer	Boeing Integrated Defense Systems
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	Williams International 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	B-52H Stratofortress bomber[1]

Storm Shadow/SCALP EG
Type	Long-range, air-to-surface missile
Place of origin	France, Italy, United Kingdom
Service history
In service	2002 – present
Used by	See Inventory
Production history
Manufacturer	MBDA
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	450 kg BROACH (Bomb Royal Ordnance Augmented Charge)
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	Inertial, GPS and TERPROM. Terminal guidance using imaging infrared
Launch platform	Panavia Tornado Mirage 2000 Rafale Eurofighter Typhoon (from 2015)

Ra'ad (Hatf VIII)
Type	Air-launched cruise missile (ALCM)
Place of origin	Pakistan
Service history
In service	December 2007 – Present
Used by	Pakistan Air Force
Production history
Manufacturer	Air Weapons Complex (AWC)
Unit cost	Unknown
Specifications
Weight	1,100 kg
Length	4.85 m
Warhead	450 kg HE or nuclear 10 to 35 kt[1]
Engine	Turbofan
Operational range	350 km
Speed	Subsonic
Guidance system	INS, TERCOM, DSMAC, GPS,COMPASS
Launch platform	Combat aircraft

ASMP
Type	medium-range air to surface nuclear missile
Place of origin	France
Service history
In service	1986
Production history
Manufacturer	Aérospatiale
Specifications
Weight	860 kg[citation needed]
Length	5.38 m[citation needed]
Diameter	300 mm[citation needed]
Warhead	TN 81 nuclear warhead, 150 kt or 300 kt of TNT (variable yield)
Engine	liquid-fuel ramjet
Operational range	between 80 km and 300 km[citation needed]
Speed	Mach 2 to Mach 3[citation needed]
Launch platform	Dassault Mirage IV, Dassault Mirage 2000N, Dassault Rafale, and Dassault Super Étendard

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	481 kg,[1] Mephisto (Multi-EffectPenetrator, HIgh Sophisticated andTarget Optimised)
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	Typhoon, Tornado, Gripen, F/A-18,F-15E

AGM-129 Advanced Cruise Missile
Type	Air-launched cruise missile
Service history
In service	June 1990 - 2012
Used by	US Air Force (Decommissioned)
Production history
Manufacturer	General Dynamics (initially) Raytheon Missile Systems
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	W80-1 nuclear warhead
Engine	Williams International F112-WR-100Turbofan
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	Inertial guidance system enhanced with LIDAR Terrain Contour Matching (TERCOM).
Launch platform	B-52 Stratofortress

AGM-158 Joint Air-to-Surface Standoff Missile
Type	Air-to-surface cruise missile
Place of origin	USA
Service history
In service	2009–present
Used by	United States Air Force Royal Australian Air Force Finnish Air Force
Production history
Manufacturer	Lockheed Martin
Unit cost	US$700,000(JASSM)[citation needed] 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	Global Positioning System (GPS)-aided inertial navigation system(INS)
Launch platform	B-1 Lancer B-2 Spirit B-52 Stratofortress F-15E Strike Eagle F-16 Fighting Falcon F/A-18 Hornet F/A-18E/F Super Hornet F-35 Lightning II P-3 Orion

Rafael Popeye
The "Popeye" standoff missile
Type	Air-to-surface missile
Place of origin	Israel
Service history
In service	1985 – present
Used by	See Users
Production history
Designer	Rafael Advanced Defense Systems
Manufacturer	Rafael Advanced Defense Systems Lockheed Martin Turkish Aerospace Industries
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	SLBM
Place of origin	India
Service history
In service	In production (k-15)[1] 2017 (k-4)[2]
Used by	Indian Navy
Production history
Manufacturer	Defence Research and Development Organisation (DRDO) & Bharat Dynamics limited(BDL)
Produced	K-15 In production
Specifications
Weight	6[3]-7[4] tonnes (K-15) 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	Mach 7.5 (Shaurya, which is land-based version[6] of sagarika K-15 missile)[1]
Launch platform	Arihant class submarine

The K family of missiles is a series

TYPE	RANGE	Weight	Warhead	length	Status
K-15[2]	750 km-1,500 km	6[3]-7 tonnes[4]	1 tonne	10 m	K-15/B-05 in series production. Land-based missile awaiting clearance. Tests completed.[3][8]
K-4 Mark I [2][5]	3,500 km	20 tonnes[5]	2.5 tonnes[5]	10 m	First tested from a depth of 30 meters on 24 March 2014. More tests expected before being getting operational.[9][10][11]
K-4 Mark II	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	Under Development by DRDO[13][14]

SOM Cruise Missile
SOM cruise missile mockup exhibited during MSPO 2014 at Kielce, Poland.
Type	Cruise missile Anti-ship missile
Place of origin	Turkey
Service history
In service	Since 2012
Production history
Manufacturer	TÜBİTAK-SAGE and Roketsan
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	250 km (130 nmi)[2] (operational variant)[3] 300 kilometres (162 nmi) (tested range) 500 kilometres (270 nmi) (claimed range)
Flight altitude	Terrain hugging Sea skimming
Speed	623 knots (0.94 Mach )
Guidance system	INS / GPS Terrain Referenced Navigation Image Based Navigation Automatic Target Recognition Imaging Infrared Seeker[4]
Accuracy	5 metres (16 ft) CEP
Launch platform	F-16 Fighting Falcon F-4 Phantom II