Standoff Missiles

BLACKEAGLE

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Standoff missiles are missiles or bombs which may be launched at a distance sufficient to allow attacking personnel to evade defensive fire from the target area. Typically, they are used against land- and sea-based targets in an offensive operation. The name is derived from their ability to engage the target while standing off outside the range at which the defenders are likely to engage the attacker. Typical stand-off weapons include cruise missiles, glide bombs and short-range ballistic missiles.

Types of missiles

ASMP

wum537.jpg


Type medium-range air to surface nuclear missile
Place of origin France
In service 1986
Manufacturer Aérospatiale
Specifications
Weight
860 kg
Length 5.38 m
Diameter 300 mm
Warhead TN 81 nuclear warhead, 150 kt or 300 kt of TNT
Engine liquid-fuel ramjet

Operational range

between 80 km and 300 km
Speed Mach 2 to Mach 3

Launch platform

Dassault Mirage IV, Dassault Mirage 2000N, Dassault Rafale, and Dassault Super Étendard

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AGM-28 Hound Dog

AGM-28_Hound_Dog.jpg



Type Cruise Missile
Place of origin United States
In service September 13, 1960
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

Astro-inertial guidance

Launch platform

B-52 Stratofortress.
AGM28_592820.jpg


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GAM-87 Skybolt

IMG_0490.JPG

Type Air-launched ballistic missile
Manufacturer Douglas Aircraft, Northrop
Specifications
Weight
11,000 pounds (5,000 kg)
Length 38 feet 3 inches (11.66 m)
Diameter 35 inches (890 mm)
Warhead W59 thermonuclear (1 Mt)
Engine Aerojet General two-stage solid-fueled rocket
Wingspan 5 feet 6 inches (1.68 m)

Operational range

1,150 miles (1,850 km)
Flight ceiling 480 km
Speed 9,500 miles per hour (15,300 km/h)

Guidance system

inertial guidance

Launch platform

Aircraft
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AGM-69 SRAM

090403-F-1234P-014.jpg


Type Nuclear air-to-surface missile
Place of origin United States
In service 1972–1993
Used by United States
Wars Cold War
Production history
Designer
Boeing
Designed 1965
Manufacturer Boeing
Unit cost $592,000
Produced 1971–1975
Number built 1,500
Specifications
Weight
2,230 lb (1,010 kg)
Length 15 ft 10 in (4.83 m) w/ tail fairing,
14 ft 0 in (4.27 m) without
Diameter 17.5 in (0.44 m)
Warhead W69 nuclear warhead
Blast yield
  • 17 kilotons (fission)
  • 210 kilotons (fusion)
Engine Lockheed SR75-LP-1
two-pulse solid-fueled rocket

Operational range

110 nautical miles (200 km)
Speed Mach 3

Guidance system

General Precision/Kearfott KT-76 Inertial measurement unit
Accuracy 1,400 ft (430 m)
Transport Airplane

MKU-Kickback-Backfire-C-1S.jpg


 

BLACKEAGLE

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AGM-86 ALCM

agm-86c.jpg


Type Air-to-ground strategic cruise missile
Place of origin United States
In service 1982-present
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
Produced 1980
Number built 1,715 (AGM-86B), 239 (AGM-86C), 50 (AGM-86D)
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)
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)
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

Boeing B-52H Stratofortress

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AGM-154 Joint Standoff Weapon

ORD_AGM-154_JSOW_Free-fall_lg.jpg

Type Glide bomb
Manufacturer Raytheon
Unit cost AUPP AGM-154A: $282,000
AGM-154B: $484,167
AGM-154C: $719,012
Specifications
Weight
483 to 497 kg (1,065 to 1,095 lb)
Length 410 cm (160 in)
Diameter 330 mm (13 in)
Warhead BLU-97/B - Combined Effects Bomblets (JSOW A)
BLU-108 - Sensor fused weapon (JSOW B - now cancelled)
BROACH multi-stage warhead (JSOW C)
Wingspan 270 cm (106 in)

Operational range

low altitude release: 22 kilometres (12 nmi)
high altitude release: 130 kilometres (70 nmi)
990219N0800C003.jpg



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AGM-158 JASSM

ORD_AGM-158_JASSM_Flight_Side_lg.jpg

Type Air-to-surface cruise missile
Place of origin United States
Service history
In service
2009–present
Used by United States Air Force
Royal Australian Air Force
Finnish Air Force
Polish Air Force
Manufacturer Lockheed Martin
Unit cost US$700,000(JASSM)
US$1.327m(JASSM-ER FY13)
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
agm-158-jassm-6.jpg


 

BLACKEAGLE

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Storm Shadow

Stormshadow01.jpg


Type
Long-range, air-to-surface missile
Place of origin France, Italy, United Kingdom
In service 2002 – present
Used by See Inventory
Production history
Manufacturer
MBDA
Unit cost £790,000
Specifications
Weight
1,300 kilograms (2,866.0 lb)
Length 5.1 metres (16.7 ft)
Diameter 0.48 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

300+nm (560+km) Lo-Lo profile http://en.wikipedia.org/wiki/Storm_Shadow#cite_note-3
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 DSMAC

Launch platform

Panavia Tornado
Mirage 2000
Rafale
Eurofighter Typhoon (from 2015)

typhoon.jpg


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SOM (missile)

t.jpeg


Type Cruise missile
Anti-ship missile
Place of origin Turkey
Service history
In service
Since 2012
Production history
Manufacturer
TÜBİTAK-SAGE and Roketsan/ SOM-J to be additionally produced by Lockheed Martin under licence from 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
SOM-J: Semi-armour piercing type with blast/fragmentation
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]
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
F-35 Lightning II
som_banner_940.jpg


 

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Hatf-VIII (Ra'ad)

4-29-2011_14855_l.jpg


Type Air-launched cruise missile (ALCM)
Place of origin Pakistan
In service December 2007 – Present
Used by Pakistan Air Force
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
Engine Turbofan

Operational range
350 km
Speed Subsonic

Guidance system
INS, TERCOM, DSMAC, GPS, COMPASS

Launch platform
Combat aircraft

Raad_Mirage.jpg


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AS-16 Kickback

ch15_102.jpg


Type air-to-surface missile
antitank missile
Place of origin Soviet Union
In service 1988
Used by Russia
Designer Raduga
Designed 1970s-1980s
Specifications
Weight
1,200 kg (2,650 lb)
Length 478 cm (15 ft 8 in)
Diameter 45.5 cm (17.9 in)
Warhead weight 150 kg (331 lb)
Wingspan 92 cm (36.2 in) maximum

Operational range
300 km (160 nmi)
Speed Up to Mach 5

Guidance system
inertial guidance, active radar homing, or anti-radiation missile

Launch platform
Tu-95MS-6, Tu-22M3, and Tu-160
as16.jpeg

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Kh-55

kh-55.jpg


Type Air-launched strategic cruise missile
Place of origin Soviet Union
In service 1983-present
Used by Russia, China, Iran
Wars no evidence of combat use
Designed 1971-1981
Manufacturer Raduga OKB
Unit cost unknown
Produced 1981
Specifications
Weight
1,650 kg (3,640 lb) (Kh-65SE)
2,400 kg (5,300 lb) (Kh-101)
Length 604 cm (19 ft 10 in) (Kh-65SE)
745 cm (24 ft 5 in) (Kh-101)
Diameter 51.4 cm (20.2 in) (Kh-55-Kh-55SM)
Warhead Nuclear or Conventional warhead
Blast yield Nuclear 200kt (Kh-55-Kh-55SM)
Engine turbofan (Kh-55-Kh-55SM)
400 kgf (Kh-55-Kh-55SM)
Wingspan 310 cm (122.0 in) (Kh-55-Kh-55SM)
Propellant jet fuel

Operational range
2,500 km (1,300 nmi) (Kh-55)
3,000 km (1,600 nmi) (Kh-55SM)
600 km (320 nmi)(Kh-65SE)
300 km, later 600 km(Kh-SD)
Flight altitude under 110 m/300 ft
Speed Mach 0.75 (KH-SD)
Mach 0.6-0.78 (Kh-101)

Guidance system
inertial guidance with Doppler radar/terrain map updates; Kh-SD had a TC/IIR terminal guidance system, and an alternative active radar homing seeker was proposed

Launch platform
Tu-95MS, Tu-160, Su-34
000-Kh-55-Tu-160-1S.jpg


 

BLACKEAGLE

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AS-6 Kingfish

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Tu-16_Badger_G.jpg

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Kh-22

KH22.jpg


Type air-to-surface missile
Place of origin Soviet Union
Used by Russia
Manufacturer Raduga
Produced 1962
Specifications
Weight
5,820 kg (12,800 lb)
Length 11.65 m (38.2 ft)
Diameter 92 cm (36 in)
Warhead 1,000 kg (2,205 lb) RDX
or 350–1000kt nuclear
Engine Liquid-fuel rocket
Wingspan 300 cm (120 in)
Propellant Tonka-250 and IRFNA

Operational range

600 km (320 nmi) (Kh-22M/MA)
Flight ceiling 10-14km or 27km
Speed Mach 4.6

Guidance system

Inertial guidance followed by terminal active radar homing

Launch platform

Tu-22M, Тu-22К, Тu-95К22

zhrp.jpg
 

Legend

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#6
Good work @BLACKEAGLE

Very informative thread.

I have a question if you may. Are these effective against moving targets?
 

BLACKEAGLE

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Good work @BLACKEAGLE

Very informative thread.

I have a question if you may. Are these effective against moving targets?
They're not made for moving targets in the first place, they're used for well protected, valuable and strategic stationary targets.
 
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wow these missiles are absolutely no joke their ability to cause havoc in pain is like no other I haven't seen results like this in a long period of time.
 

Kjordo711

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Nothing like some pictures of missiles to spice up your day. Especially that Storm Shadow. Just thinking about the amount of damage that could do, really makes you think. Plus the design of the missile is just so damn beautiful. If that was the last thing I saw dropping on me I would find it beautiful to watch plummet down to me from the air.
 
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