Friday, September 24, 2010

Surface To Air/Air Defence,Akash


Surface To Air/Air Defence

Akash

Akash (Sanskrit: आकाश Ākāś "Sky") is India's medium range surface-to-air missile defense system developed by the Defence Research and Development
  (DRDO) and Bharat Electronics Limited(BEL) as part of the Integrated Guided Missile Development Program. The missile can target aircraft up to 30 km away, at altitudes up to 18,000 m. Akash can be fired from both tracked and wheeled platforms.is said to be capable of both conventional and nuclear warheads, with a reported payload of 60 kg. A nuclear warhead could potentially give the missile the capability to destroy both aircraft and warheads from ballistic missiles. The missile battery is described as being able to track and attack several targets simultaneously.
Akash
Akash SAM.jpg
An Akash missile being test fired from the Integrated Test Range (ITR), Chandipur, Orissa.
TypeSurface-to-air missile
Place of origin India
Production history
DesignerDRDO
ManufacturerBharat Electronics Limited, Bharat Dynamics Limited
Produced2009
Number builtIAF: 1000 missiles, IA: 1000 missiles
Specifications (Akash missile)
Weight720 kg
Length5.78 m
Diameter
35 cm



WarheadDigital proximity fuse is coupled with a 55 kg pre-fragmented warhead
Warhead weight55 kg
Detonation
mechanism

Number of threats Destroyed

Area Covered
RF Proximity


16


2000km sq

PropellantIntegrated Ramjet Rocket Engine.
Operational
range
25-30km
Flight altitude18 km
SpeedMach 2.5


Organisation
An Akash battery comprises four 3D phased array radars and four launchers with three missiles each, all of which are interlinked. Each radar is able to track 16 targets simultaneously and control a launcher with 3 missiles. Hence it is reported to be able to track 64 targets and simultaneously attack any 12 of those targets at one time. The Akash system is comparable to the Patriot system, but unlike the Patriot, Akash is fully mobile and capable of protecting a moving convoy of vehicles. Like the Patriot, the Akash is really an air defence SAM which has been tested in a ballistic missile role. The system provides air defence missile coverage of 2,000 km².
The India military's combined orders of the Akash, including radar systems(WLR and Surveillance), have a total worth of $5.2 billion (Indian rupee 23,300 crore)

Development and history

The first test flight of Akash missile was conducted in 1990, with development flights up to March 1997.
Two Akash missiles intercepted two fast moving targets in simultaneous engagement mode in 2005. 3-D Central Acquisition Radar (3D-CAR) group mode performance is also fully established.
Along with India, a limited number of other countries including the US, Russia, Japan, Israel, and some EU countries have developed operational multitarget-handling surface-to-air missile systems. With the successful user trials of Akash, India has validated the technology and operational efficacy of this missile system. This system is claimed to be more accurate than the MIM-104 Patriot as it has thrust during the entire course of its flight compared to the Patriot that has thrust only for the first 12 seconds, after which the missile coasts, thus making it less accurate. Apart from that the Akash can be launched from static or mobile platforms, including a battle tank. \The Akash Missile Development cost of Indian rupee 1,000crore ($200 million), including the project sanction of Indian rupee 600 crore ($120 million), is 8-10 times lower than the cost of similar system developments in so called advanced countries. Akash, which is considered as Indian ‘poor man’s Patriot,’ has certain unique characteristics like mobility, all-the-way-powered flight till target interception, multiple target handling, digitally-coded command guidance and fully automatic operation.”.

Akash Mk-2

Development work for Akash Mk-2 variant has begun, since recently Ministry of Defence officially granted funds and permission for its further development.DRDO is confident to field and test new Akash Mk-2 within 3 year period, major changes that Akash MK-2 will have is the range of missile, Army and Air force wants Akash MK-2 to have range of 40 to 60 km from its current range (Akash MK-1) of just 25 km. for that DRDO has been working on using better composite booster with lengthened booster section to achieve the desired range .Akash MK-1 is guided by phased array fire control radar called Rajendra BSR (Battery Surveillance Radar) which is PESA radar, while Akash Mk-2 will have a Rajendra derivative AESA radar to perform the same role, AESA radar will give it better tracking, and engagement functions. Work on AESA variant has begun and almost nearing completion

Description

Akash is a surface-to-air missile with an intercept range of 30 km. It has a launch weight of 720 kg, a diameter of 35 cm and a length of 5.78 metres. Akash flies at supersonic speed, reaching around Mach 2.5. It can reach an altitude of 18 km and can be fired from both tracked and wheeled platforms. An on-board guidance system coupled with an actuator system makes the missile maneuverable up to 15g loads and a tail chase capability for end game engagement. A digital proximity fuse is coupled with a 55 kg pre-fragmented warhead, while the safety arming and detonation mechanism enables a controlled detonation sequence. A self-destruct device is also integrated. It is propelled by an Integrated Ramjet Rocket Engine. The use of a ramjet propulsion system enables sustained speeds without deceleration throughout its flight. The Missile has command guidance in its entire flight.
The design of the missile is somewhat similar to that of the SA-6 with four long tube ramjet inlet ducts mounted mid-body between wings. For pitch/yaw control four clipped triangular moving wings are mounted on the mid-body. For roll control four inline clipped delta fins with ailerons are mounted before the tail. However, the internal schema shows a different layout with an onboard digital computer, no Semi-active seeker, different propellant, different actuators and command guidance datalinks. The Akash carries an onboard radio-proximity fuse.

System

Each Akash battery consists of four self-propelled Launchers (3 Akash SAMs each), a Battery Level Radar - the Rajendra, and a Command post (Battery Control Centre). Two batteries are deployed as a Squadron (Air Force), while up to four form an Akash Group (Army configuration). In both configurations, an extra Group Control Centre (GCC) is added, which acts as the Command and Control HQ of the Squadron or Group. Based on a single mobile platform, GCC establishes links with Battery Control Centres and conducts air defense operations in coordination with air defense set up in a zone of operations.
For early warning, the GCC relies on the Central Acquisition Radar. However, individual batteries can also be deployed with the cheaper, 2-D BSR (Battery Surveillance Radar) with a range of over 100 km.
Each Akash battery can engage up to four targets. Each battery has four launchers with three missiles each, with each Rajendra able to guide four missiles in total, with a maximum of two missiles per target. Up to a maximum of four targets can be engaged by a typical battery with a single Rajendra if one missile is allotted per target.
Communications between the various vehicles are a combination of wireless and wired links. The entire system is designed to be set up quickly and to be highly mobile for high survivability.
The Akash system can be deployed by rail, road or air.

Hypersonic Boost Glide Missile, Shaurya Missile


Shaurya Missile

The Shaurya missile (Sanskrit: Valour) is a canister launched hypersonic surface-to-surface tactical missile developed by the Indian Defence Research and Development Organization (DRDO) for use by the Indian Armed Forces. It has a range of between 750 to 1900 km and is capable of carrying a payload of one-tonne conventional or nuclear warhead. It gives the potential to strike in the short-intermediate range against any adversary. The Shaurya missile provides India with a significant second strike capability
Shaurya
Shaurya Missile.jpg
Shaurya Missile first test launch
TypeHypersonic Boost Glide Missile
Place of originIndia
Service history
Used byIndian Armed Forces
Production history
ManufacturerDefence Research and Development Organisation (DRDO)
Specifications
Speed
Range
Warhead
Weight
6000 km/hr
1900 km
1 tonne nuclear/conventional
6.2 ton
Height10 m
Diameter0.74 m

Description
The Shaurya missile is speculated to be the land version of the under-water Sagarika K-15 missile, although DRDO officials have reportedly denied its connection with the K-15 program Shaurya is stored in a composite canister, which makes it much easier to store for long periods without maintenance as well as to handle and transport. It also houses the gas generator to eject the missile from the canister before its solid propellant motors take over to hurl it at the intended target.
Shaurya missiles can remain hidden or camouflaged in underground silos from enemy surveillance or satellites till they are fired from the special storage-cum-launch canisters. DRDO scientists admit that given Shaurya's limited range at present, either the silos will have to be constructed closer to India's borders or an extended range version will have to be developed. The Shaurya system will require some more tests before it becomes fully operational in two to three years. Moreover, defence scientists say the high-speed, two-stage Shaurya is highly maneuverable which also makes it less vulnerable to existing anti-missile defence systems. Shaurya can reach a velocity of Mach 6 even at low altitudes. On November 12, the missile reached a velocity of Mach 5 as it crossed a distance of 300 km, with a surface temperature of 700{+0} Celsius. The missile performed rolls to spread the heat uniformly on its surface. Flight time is between 500 seconds and 700 seconds. It has been described as a complex system with high-performance navigation and guidance systems, efficient propulsion systems, state-of-the-art control technologies and canisterised launch. It can be easily transported by road and launched by TEL. The missile, encased in a canister, is mounted on a single vehicle, which has only a driver’s cabin, and the vehicle itself is the launch platform. This “single vehicle solution” reduces its signature – it cannot be easily detected by satellites – and makes its deployment easy.The gas generator, located at the bottom of the canister, fires for about a second and a half. It produces high pressure gas, which expands and ejects the missile from the tube. The missile has six motors; the first one is the motor in the gas generator.The centerpiece of a host of new technologies incorporated in Shourya is its ring laser gyroscope and accelerometer. The ring laser gyroscope was tested & integrated by the Research Center Imarat (RCI) based in Hyderabad.
Shaurya missile was revealed to be designed specifically to be fired from submarines. Top DRDO scientist has confirmed this and said that this missile after taking off and reaching a height of about 50 km will start flying like a Hypersonic cruise missile. Once it reaches the target areas it maneuvers towards the target before striking with an accuracy of 20 to 30 m within the target area.

First test

The missile was first test fired on November 12, 2008. The missile was launched from an underground facility with an in-built canister from Complex-3 of the Integrated Test Range at Chandipur.

Wednesday, September 22, 2010

ICBM. Surya 1.Surya 2

Surya 1

The Surya missile is a speculation about an Inter Continental ballistic missile being developed by India. The first report about the Surya missile was published by the Nonproliferation review in 1995.



chandrayaan 1, isro, pslv, surya missile

History

According to a report published in The Nonproliferation Review, in the Winter of 1995, Surya (meaning the Sun in Sanskrit and many Indian languages) is the codename for the first Intercontinental Ballistic Missile that India is reported to be developing. The DRDO is believed to have begun the project in 1994. This report has not been confirmed by any other sources until 2010. Officials of the Indian government have repeatedly denied the existence of the project.
According to the report, the Surya is an intercontinental-range, surface-based, solid and liquid propellant ballistic missile. The report further adds that Surya is the most ambitious project in India's Integrated Guided Missile Development Programme.The Surya is speculated to have a range between 12,000 to 16,000 kilometers.
As the missile is yet to be developed, the specifications of the missile are not known and the entire program continues to remain highly secretive. Estimates of the range of this missile vary from 12,000 kms to 16,000 kms. It is believed to be a three-stage design, with the first two stages using solid propellants and the third-stage using liquid. In 2007, the Times of India reported that the DRDO is yet to reveal whether India's currently proposed ICBM will be called Agni-V (or Surya-1). As of 2009 it was reported that the government had not considered an 8,000-km range ICBM.

Design

Sources say the DRDO's most treasured dream -- denied in public -- remains the development of an ICBM with a range of 15,000 kilometres, already christened Surya or sun, to match Chinese DF-3 ICBMs that can hit US cities."DRDO scientists are working on miniaturising systems of Agni-III so that a third stage can be squeezed into the 16-metre-long missile to enable it to go up to 5,500 kilometres with the same 1.5-tonne payload,"DRDO chief M. Natarajan told reporters in New Delhi.

Speculated specifications

  • Class: ICBM
  • Lasing: "Surface based",Underwater based in certain strategic areas & "Submarine" based is its most important aspect which may range upto 12,000 kms
  • Length: 40.00 m
  • Diameter: 2.8 m
  • Launch Weight: 80,000 kg
  • Propulsion: First/second stage solid, third liquid
  • Warhead Capabilities: 3-10 nuclear warheads of 250-750 kilotons each
  • Status: Development / Developed to be tested
  • In Service: 2015
  • Range: 12,000 - 16,000 km

The Surya-1 is an intercontinental-range, surface-based, solid and liquid propellant ballistic missile under development. It is based upon a space launch vehicle being developed by India’s space program
to improve the nation’s aerospace industry. This project would result in India’s first intercontinental-range ballistic missile.

The Surya-1 and -2 will be classified as a strategic weapon. It will likely be used to extend the Indian nuclear deterrent force to targets deeper within China. India can only hit a limited number of targets within China, even upon the completion of the Agni-3 missile. The development of a true ICBM would make almost any strategic target within China vulnerable and decrease India’s relative weakness. This would develop a credible deterrent for India against any Chinese aggression.


The Surya-1 will have an expected range of some 8,000 km (4971 miles). It reportedly has a length of 40 m and a launch weight of 80,000 kg. As the missile has yet to be developed, the payload and warhead are as yet unknown. It is believed to be a three-stage design, with the first two stages using solid propellant and the third-stage using liquid.

Surya 2

Speculated specifications

  • Class: ICBM
  • Lasing: "Surface based",Underwater based in certain strategic areas & "Submarine" based is its most important aspect which may range upto 20,000 kms
  • Length: 40.00 m
  • Diameter: 2.8 m
  • Launch Weight: 60,000+ kg
  • Propulsion: First/second stage solid, third liquid
  • Warhead Capabilities: 2-8 nuclear warheads of 250-750 kilotons each
  • Status: Development
  • In Service: 2016
  • Range: 15,000 - 20,000 km

AAD and PAD Programme

 AAD and PAD Programme



Under former president Dr. Abdul Kalam India pursued the Integrated Guided Missile Development Program (IGMDP) which was an Indian Ministry of Defense program for the development of a comprehensive range of missiles, including the intermediate range Agni missile (Surface to Surface), and short range missiles such as the Prithvi ballistic missile (Surface to Surface), Akash missile (Surface to Air), Trishul missile (Surface to Air) and Nag Missile (Anti Tank). Other projects such Indian Ballistic Missile Defense Program have derived from the IGMDP. In 2005, India became only the fourth country to have Anti Ballistic capability when India tested two systems the AAD and PAD.

India has methodically built an indigenous missile production capability, using its commercial space-launch program to develop the skills and infrastructure needed to support an offensive ballistic missile program. For example, during the 1980s, India conducted a series of space launches using the solid-fueled SLV-3 booster. Most of these launches put light satellites into near-earth orbit. Elements of the SLV-3 were subsequently incorporated into two new programs. In the first, the new polar-space launch vehicle (PSLV) was equipped with six SLV-3 motors strapped to the PSLV's first stage. The Agni IRBM technology demonstrator uses the SLV-3 booster as its first stage.

Indian Balastic Missiles,Prithvi

Indian Balastic Missiles
Prithvi
Prithvi
PAD integration.JPG
Prithvi SRBM (Short-range ballistic missile)
TypeShort Range Ballistic Missile
Place of originIndia
Service history
In service1994 (Prithvi I)
Used byIndian Army
Indian Air Force
Indian Navy
Production history
ManufacturerDefence Research and Development Organisation (DRDO)Bharat Dynamics Limited (BDL)
ProducedFebruary 25, 1988 (Prithvi I)
January 27, 1996 (Prithvi II)
April 11, 2000 (Dhanush)
January 23, 2004 (Prithvi III)
Specifications
Weight4,400 kg (Prithvi I)
4,600 kg (Prithvi II)
5,600 kg (Prithvi III)
Length9 m (Prithvi I)
8.56 m (Prithvi II, Prithvi III)
Diameter110 cm (Prithvi I, Prithvi II)
100cm (Prithvi III)


EngineSingle Stage liquid fuel dual motor(Prithvi I, Prithvi II),
Single Stage Solid Motor (Prithvi III)
Operational
range
150 km (Prithvi I)
250 km (Prithvi II)
350 - 600 km (Prithvi III)
Guidance
system
strap-down inertial guidance
Launch
platform
8 x 8 Tatra Transporter Erector Launcher

Prithvi (Sanskrit: पृथ्वी, pṛthvī "Earth") is a tactical surface-to-surface, short-range ballistic missile (SRBM) developed by DRDO of India under the Integrated Guided Missile Development Program.

Development and History

The Government of India launched the Integrated Guided Missile Development Program in 1983 to achieve self sufficiency in the development and production of wide range of Ballistic Missiles, Surface to Air Missiles etc.
Prithvi was the first missile to be developed under the Program. DRDO attempted to build Surface-to-air Missile under Project devil
Variants make use of either liquid or both liquid and solid fuels. Developed as a battlefield missile, it could carry a nuclear warhead in its role as a tactical nuclear weapon.

Variants

The Prithvi missile project encompassed developing 3 variants for use by the Indian Army, Indian Air Force and the Indian Navy. The initial project framework of the Integrated Guided Missile Development Program outlines the variants in the following manner.
Prithvi I (SS-150) - Army Version (150 km range with a payload of 1,000 kg)
  • Prithvi II (SS-250) - Air Force Version (250 km range with a payload of 500 kg)
  • Prithvi III (SS-350) - Naval Version (350 km range with a payload of 500 kg)
  • Dhanush- Dhanush is reportedly a naval version of Prithvi which can be launched from Ships. Some sources claim that Dhanush is a System consisting of stabilization platform and missiles, which has the capability to launch both Prithvi II and Prithvi III from Ships while others report that Dhanush is a variant of Prithvi-II Ballistic Missile.
Over the years these specifications underwent a number of changes. While the codename Prithvi stands for any missile inducted by India into its armed forces in this category, the later developmental versions are codenamed as Prithvi II and Prithvi III.

Description

Prithvi I

Prithvi I class was a surface-to-surface missile having a maximum warhead mounting capability of 1,000 kg, with a range of 150 km. It has an accuracy of 10 – 50 metres and can be launched from Transporter erector launchers. This class of Prithvi missile was inducted into the Indian Army in 1994.























Prithvi II

Prithvi II class is also a single stage liquid-fuelled missile having a maximum warhead mounting capability of 1,000 kg, but with an extended range of 250 kilometres. It was developed with the Indian Air Force being the primary user. It was first test-fired on January 27, 1996 and the development stages were completed in 2004. The Prithvi II class of missiles are in the process of induction by the Indian Airforce. In a recent test, the Missile was launched with an extended range of 350 kilometres and improved Aided Inertial Navigation. The missile has the features to deceive Anti Ballistic Missiles. According to news sources the range is now increased to 350kms

 

 

 

Prithvi III



Prithvi III class (codenamed Dhanush meaning Bow) is a two-stage ship-to-surface missile. The first stage is solid fuelled with a 16 metric ton force (157 kN) thrust motor. The second stage is liquid fuelled. The missile can carry a 1,000 kg warhead to a distance of 350 km and a 500 kg warhead to a distance of 600 kilometres and a 250 kilogram warhead up to a distance of 750 kilometres. Dhanush is a system consisting of a stabilization platform (Bow) and the Missile (Arrow). Supposedly it is a customised version of the Prithvi and that the additional customizations in missile configuration is to certify it for sea worthiness. Dhanush has to be launched from a hydraulically stabilized launch pad. Its low range acts against it and thus it is seen a weapons either to be used to destroy an aircraft carrier or an enemy port. The missile has been tested from the surface ships many times
Prithvi III was first tested in 2000 from INS Subhadra, a Sukanya class patrol craft. The missile was launched from an updated, reinforced helicopter deck of the vessel. The first flight test of the 250 km variant was only partially successful. The full operational testing was completed in 2004 The following year in December an enhanced 350 km version of the missile was tested from the INS Rajput and successfully hit a land based target. The missile was again successfully tested-fired from INS Subhadra anchored about 35 km offshore from the Integrated Test Range at Chandipur on December 13, 2009. It was the sixth test of the missile.

Cruise Missile Moskit

Cruise Missile
Moskit
India has most probably bought both land and ship variants which have a range of 120 km. India bought around 200 Klub missiles and now it is believed that the Moskit have been kept in reserve but can still be used.
 
Moskit
Moskit missile.jpg
TypeAnti-ship missile
Production history
ManufacturerMKB Raduga
Specifications
Weight4,500 kg
Length9.745 m
Diameter0.8 m

Warhead320 kg high explosive or 120 kt of TNT fission-fusion thermonuclear


EngineFour ramjets (solid fuel rocket on air-to-surface version)
Wingspan2.10 m
Operational
range
120 km
Flight altitude20 m above sea level
SpeedMach 2.5
Guidance
system
active radar
Launch
platform
naval ships, fixed-wing aircraft



The P-270 Moskit (Russian: П-270 «Москит»; English: Mosquito) is a Russian supersonic ramjet powered cruise missile. Its GRAU designation is 3M80, and its NATO reporting name is SS-N-22 Sunburn. The missile system was designed by the Raduga Design Bureau during the 1970s as a follow up to the SS-N-9 "Siren". The Moskit was originally designed to be ship launched, but variants have been adapted to be launched from land (modified trucks), underwater (submarines) and air (reportedly the Sukhoi Su-33, a naval variant of the Sukhoi Su-27). The missile can carry conventional and nuclear warheads.
The exact classification of the missile is unknown, with varying types reported; this has been due to the secrecy surrounding an active military weapon. It is one of the missiles known by the NATO codename SS-N-22 Sunburn. It reaches Mach 3 at a high altitude and its maximum low-altitude speed is M2.2, triple the speed of the subsonic American Harpoon. When such slower missiles, like the Harpoon or the French Exocet are used, the maximum theoretical response time for the defending ship is 120-150 seconds. This provides time to launch countermeasures and employ jamming before deploying "hard" defense tactics such as launching missiles and using quick-firing artillery. But the 3M82 "Mosquito" missiles are extremely fast and give the defending side a maximum theoretical response time of merely 25-30 seconds, rendering it extremely difficult to employ jamming and countermeasures, let alone fire missiles and quick-firing artillery. The Moskit was designed to be employed against smaller NATO naval groups in the Baltic Sea (Danish and German) and the Black Sea (Turkish) and non-NATO vessels in the Pacific (Japanese, South Korean, etc.), and to defend the Russian mainland against NATO amphibious assaultThe missile has been purchased by the People's Liberation Army Navy (China), and reported to be purchased by Iran.

Cruise Missile P-70 Ametist

Cruise Missile


P-70 Ametist
India has acquired around 50+ all are reserved due to short range but are ready to be used since last upgradation in 90's 
 
Type
Anti-shipping missile
Place of origin
Soviet Union
Service history
In service
1968-1995
Used by
Russia, India
Production history
Manufacturer
Specifications
Weight
7,700 lb (3,500 kg)
Length
23.0 ft (7.0 m)
Warhead
HE or 200kt nuclear
Warhead weight
1,170 lb (530 kg)
Propellant
Solid fuel
Operational
range
65 km (35 nmi)
Speed
Mach 0.9
Launch
platform


















































The P-70 Ametist (NATO reporting name SS-N-7 Starbright, GRAU designation 4K66; Russian: П-70 «Аметист» 'Amethyst') was an anti-shipping missile carried by Soviet Charlie-I submarines. A sub-launched version of the SS-N-2 'Styx', it was soon succeeded by the P-120 Malakhit (SS-N-9 'Siren').
Design
The P-15M was fitted with an L band sensor and a new altimeter radar both developed for the 'Siren', but there was no room for a datalink in the smaller 'Styx'. Folding wings were added to reduce the size of the missile, and the missile can be launched at a maximum depth of 30 meter.
The short range of the P-70 meant that it did not need mid-course updates from a radar on the submarine, so it could be fired whilst submerged. This more than made up for its lack of range compared to the 'Shaddock'.
Operational history
The P-70 went into service with the Soviet Navy on the first Charlie I, on June 3, 1968. About 200 were produced.
India leased the Chakra, a Soviet Charlie I submarine from January 1988 to 1992, to gain experience of operating a nuclear submarine.
Operators