Sunday, September 14, 2014

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 1.jpg
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
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


AGM-86

ALCMCruiseMissile.JPG
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

Storm Shadow

Type
Place of origin
Service history

In service
2002 – present
Used by
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
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
Eurofighter Typhoon (from 2015)

Ra'ad (Hatf VIII) Dassault Mirage IIIDP with Ra'ad missile.png

Type
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

Air-sol moyenne portée (ASMP).png

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
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


TAURUS KEPD 350

Taurus KEPD 350.jpg

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


AGM-129 Advanced Cruise Missile

Agm-129 acm.jpg

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

Agm-158 JASSM.jpg

Type
Air-to-surface cruise missile
Place of origin
Service history

In service
2009–present
Used by
Production history

Manufacturer
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
Launch
platform


Rafael Popeye

Popey missile.jpg
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
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

The K family of missiles is a series
TYPE
RANGE
Weight
Warhead
length
Status
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]
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]
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 on MSPO 2014.jpeg
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
250 km (130 nmi)[2] (operational variant)[3]
300 kilometres (162 nmi) (tested range)
500 kilometres (270 nmi) (claimed range)
Flight altitude
Speed
623 knots (0.94 Mach )
Guidance
system
INS / GPS
Image Based Navigation
Accuracy
5 metres (16 ft) CEP
Launch
platform

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