Pics of people whom you appreciate most....

by shayar_dildaar on April 19, 2006, 05:07:28 AM
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shayar_dildaar
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«Reply #135 on: April 25, 2006, 05:41:20 PM »
Chal Indian governement k liye chori karte hain America se...Cool man, we need to pump in money for knowing the Technology inside..............




Quote from: "indian_groom"
HARRIER..........NO NEED OF RUN WAY TO FLY.

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indian_groom
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«Reply #136 on: April 25, 2006, 05:42:13 PM »
Quote from: "shayar_dildaar"
Chal Indian governement k liye chori karte hain America se...Cool man, we need to pump in money for knowing the Technology inside..............




Quote from: "indian_groom"
HARRIER..........NO NEED OF RUN WAY TO FLY.








OK IM READY YAAR......................LETS DO IT
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badnaam_shayar
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«Reply #137 on: April 25, 2006, 05:44:47 PM »
MY Hero Of the Nation............Neta Ji Subhash Chandra Bose



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shayar_dildaar
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«Reply #138 on: April 25, 2006, 05:45:08 PM »
Ok Indian_groom..Kuch missiles k pic lagao yaar...
Meri jaankari zara kam hain in maamlo mein..Description bhi lagao so that we can read about it and learn at the same time..Wud apprecicate that brother..
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indian_groom
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«Reply #139 on: April 25, 2006, 09:22:34 PM »
An intercontinental ballistic missile, or ICBM, is a very long-range (greater than 5,500–km or 3,500 miles) ballistic missile typically designed for nuclear weapons delivery, i.e., delivering one or more nuclear warheads.

ICBMs are differentiated by maximum range from other ballistic missiles: intermediate-range ballistic missiles (IRBMs), short-range ballistic missiles, and the newly named theater ballistic missiles.

The following nations currently have operational ICBM systems: Russia, the United States, France [1], the United Kingdom, and People's Republic of China. India has IRBMs but is developing ICBMs . Pakistan has IRBMs but is also researching ICBMs

In 2002, the United States and Russia agreed in the SORT treaty to reduce their deployed stockpiles to not more than 2,200 warheads each.


american Intercontinental Ballistic Missile, Atlas


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indian_groom
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«Reply #140 on: April 25, 2006, 09:34:45 PM »
Since 1992. - formation RVSN VS RF, the liquidation of the missile complexes of intercontinental ballistic missiles to the territory of the Ukraine and Kazakhstan and the conclusion from Belorussia in Russia mobile BRK "poplar", rearmament of the obsolete types of missile complexes on BRK with the standardized monoblock rockets of stationary and mobile basing "Poplar- M" of the 5th generation.




and this poplor-m

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indian_groom
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«Reply #141 on: April 25, 2006, 09:42:24 PM »
India's DRDO has dedicated considerable resources to the Integrated Guided Missile Development Program. Currently this program has produced two classes of missile designs inducted into the Army and Air Force and have been deployed by specially formed missile corps. It is unclear if the Agni has been deployed, but Agni I and II are believed to have been inducted into the Army. The Agni III is scheduled for testing by year end 2005. Further, analysts believe India is developing an SLBM (Submarine-launched ballistic missile) 'Sagarika'. The Indian DRDO has successfully launched a version of the Prithvi from an underwater pontoon launcher as well as from the deck of an offshore patrol vessel indicating work on SLBM technology.

The Deccan Herald and Carnegie Endowment reported that India is developing an intercontinental ballistic missile (ICBM) called Surya. India claims the ICBM is not only "intended to deter Europe and the U.S.", but also the People's Republic of China. It is expected to have a flight range of 9,000-12,000 km.

The missile is meant as a first-strike, "derived directly from its civilian satellite launch system (the Polar Space Launch Vehicle)". It is projected to be a “three-stage ballistic missile with solid fuel rockets in the first and second stages, and a liquid propellant rocket in the third stage”. The expected launch weight of the missile could “reach 270-275 tonnes and an impact error of around 2 to 2.8 km”. The ICBM is "likely to be test-fired by 2008", and expected to be included into "the Indian armed forces’ deterrence arsenal by 2015".



The development for the intermediate-range ballistic missile, called Agni 1 (Fire), started around 1979 under the direction of the Indian Defence Research and Development Laboratory (DRDL) at Hyderabad. Agni 1 uses a first-stage motor similar to the first-stage solid rocket motor from the Indian Satellite Launch Vehicle-3 (SLV-3) based upon an earlier US Scout rocket design. SLV-3 has been used in various satellite launches since 1979. The second stage of Agni 1 uses a shortened Prithvi missile liquid-propellant motor system.
    There were conflicting reports in 1995 concerning the Agni programme. One report suggested that the programme had been halted due to technical difficulties. The second report suggested that the Indian government was planning a further five test launches. However, in December 1996, the Indian government announced that the Agni 1 trials programme would be terminated, but in July 1997, the development programme was restarted. It seems likely that the programme was restarted as a result of the development of new solid-propellant ballistic missiles in China.
     There are reported to be four Agni versions in production or development; Agni 1 with a range of 2,500 km, Agni 2 with a range 3,000 km, Agni 2 upgrade with a range of 3,500 km, and Agni 3 with a range of 5,000 km. A range of around 4,000 km would be required for a missile to reach Beijing from India. An Agni-2 missile was displayed in January 1999 and the first test launch was made in April 1999. Agni 2 is a two-stage solid-propellant missile. A new first-stage solid motor with a diameter of 1.8 m and carrying 36,000 kg of propellant is being developed, possibly for the Agni 3 missile, which is expected to use the Agni 2 as its second and third stages. An alternative approach would be to use a new third stage for Agni 3, either liquid or solid propellant. An improved optical or radar terminal phase correlation system has been developed to provide greater accuracy. The terminal guidance option could be retrofitted into existing Agni 1 missiles.
    There are unconfirmed reports that India is considering the design of an inter-continental range ballistic missile system named Surya, building on the experience of Agni and using the developed Augmented Satellite Launch Vehicle (ASLV) as its basis.

Specifications
 
Agni 1
 
Length
  21.0 m
 
Body diameter
  1.3 m (1st stage), 0.9 m (2nd stage)
 
Launch weight
  19,000 kg
 
Payload
  Single warhead; 1,000 kg
 
Warhead
  800 kg, nuclear (45 or 200 kT), chemical, HE or submunitions
 
Guidance
  Inertial with optical correlation
 
Propulsion
  Solid propellant 1st-stage; liquid 2nd-stage
 
Range
  2,500 km
 
Accuracy
  150 m CEP
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indian_groom
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«Reply #142 on: April 25, 2006, 09:46:14 PM »
The Agni programme was restarted in 1997, and, in July 1998 the Indian government announced plans to test two Agni 2 missiles. The first launch of Agni 2 was made in April 1999 from a rail car launcher located on Wheeler's Island, near Orissa in the Bay of Bengal. This flight was over a range of 2,100 km, and is reported to have carried a dummy warhead to test the safety and arming unit in real flight conditions. A second test flight was made in January 2001 from Wheeler's Island, over a range of 2,400 km, and it is believed that this launch was made from a wheeled TEL vehicle. It is believed that low-rate initial production of the Agni 2 version has been started, with an initial order for some 10 to 20 missiles. A small number (less than 5) of Agni 2 missiles are believed to have been operationally available from late 2000, and a production rate of 15 to 20 missiles a year has been suggested. Agni 3 is in full development and a first test flight is expected by 2003.





Agni 2
 
Length
  20.0 m
 
Body diameter
  1.0 m (1st and 2nd stages), 0.8 m payload
 
Launch weight
  16,000 kg
 
Payload
  Single warhead, 1,000 kg
 
Warhead
  500 kg, nuclear 200 kT
 
Guidance
  Inertial with GPS and radar correlation
 
Propulsion
  Two-stage solid propellant
 
Range
  3,000 km (2), 3,500 km (2 upgrade)
 
Accuracy
  100 m CEP
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indian_groom
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«Reply #143 on: April 25, 2006, 09:54:55 PM »
Unmanned Aerial Vehicles


India has successfully test-flown an upgraded version of its Lakshya unmanned aerial vehicle, or UAV.

Scientists from the Indian Defense Research and Development Organization, who developed the Lakshya, launched it Feb. 6 at the Integrated Test Range at Chandipur in Orissa’s coastal Balasore district, the Indo-Asian News Service reported.

The Lakshya is a subsonic reusable system remote-controlled UAV for air-to-air and ground-to-air firing practice and is designed to help train pilots and air defense personnel in engaging targets. The Lakshya was inducted into the Indian Air Force in 2000. The Navy and the Army also field Lakshyas.

The Lakshya has a range of 370 miles, a flight ceiling of 29,504 feet and a maximum speed of Mach 0.8. In 2003 India began to develop a battlefield reconnaissance version of the drone.

The drone test at the Integrated Test Range included the Lakshya in an air defense exercise to test the UAV’s accuracy in different environments.

Israel has purchased several Lakshya drones

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indian_groom
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«Reply #144 on: April 25, 2006, 09:59:50 PM »
UNMANNED AERIAL VEHICLES NISHANT

The Nishant UAV on display at Def Expo '04. The UAV has been operationalised by the Indian Army with series production scheduled to begin soon. The airframe is made of carbon/glass fibre reinforced structure which facilitates for low RCS and the drone is powered by an ALVIS AR-801 55 bhp engine driving a pusher propeller. The Vehicles R&D lab of DRDO offers two engines for generic UAV applications, namely the RE-2-21-P and RE-4-37-P power plants.
- -
 
 The 380 kg Nishant UAV requires rail-launching from a hydro-pneumatic launcher. Launches at a velocity of 45 m/sec are carried out in 0.6 seconds with 100 kW power and subsequent launches can be carried out in intervals of 20 minutes. The Mobile Hydro-Pneumatic Launcher (MHPL) system mounted on a Tatra truck weighs 14,000 kg and boasts of a life cycle of 1000 launches before requiring overhaul. Here is an example on display at Def Expo '04.
- -
 
 The Nishant UAV on static display at Aero India '03. Built to Indian Army requirements, it includes multi-mission day/night capability using advanced electro-optical payloads (CCD, FLIR and mini pan camera, SIGINT and laser rangefinder installed in a gimballed payload assembly) or the (unconfirmed) EL/M-2055 SAR/MTI UAV recon payload.
- -
 
 The Nishant UAV on display at Aero India '98. It has an endurance of 4+ hours with a 45 kg payload carrying capability, with it's integrated sensor package (FLIR, laser ranger and 35mm mini pan camera) and drive electronics contained in the Gimballed Payload Assembly (GPA), weighing 40 kg.  
- -
 
 Developed by ADE (Aeronautical Development Establishment), the Nishant UAV is primarily tasked with intelligence gathering over enemy territory and also for recce, surveillance, target designation, artillery fire correction, damage assessment, ELINT and SIGINT.



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indian_groom
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«Reply #145 on: April 25, 2006, 10:13:47 PM »
BRAHMOS is a Supersonic Cruise Missile that can be launched from submarine, ship, aircraft and land based Mobile Autonomous Launchers (MAL). The missile is launched from a Transport-Launch Canister (TLC), which also acts as storage and transportation container.

Primarily BRAHMOS is an anti-ship missile. It has the capability to engage land based targets also. The missile can be launched either in vertical or inclined position and will cover 360 degrees.

The BRAHMOS missile has identical configuration for land, sea and sub sea platforms. The air-launched version has a smaller booster and additional tail fins for stability during launch.
 
FEAUTURES

High Supersonic Velocity
  Long flight range
  Varieties of flight trajectories
  "Fire & Forget" principle
  Universal for multiple platforms
  Low Radar Signature
  Simplicity of technical operations
  High lethal power
  Higher effectiveness

ADVANTAGES

Long flight range with supersonic speed all through the flight
 Shorter flight times leading to lower target dispersion and quicker engagement
 Varieties of flight trajectories
 ‘Fire and forget’ principle of operation
 Higher destructive capability aided by the large kinetic energy of impact
 Higher effectiveness against ship defences
 Canister for transportation, storage and launch
 
 
Superiority of the BRAHMOS Supersonic Anti-ship Missile over a Subsonic Long Range Anti-ship Missile
 
In Velocity   by 3 times
In flight range   by 2.5 - 3 times
In seeker range   by 3 - 4 times
 




OPERATIONAL SCENERIO
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indian_groom
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«Reply #146 on: April 25, 2006, 10:22:40 PM »
Akash is a mobile area defense medium-range medium and high altitude surface-to-air missile with a range of 27 to 30 kilometers. Akash has a multi-target handling capability, and employs a command guidance system with provision for terminal guidance. Powered by a ram rocket propulsion and an air breathing engine, Akash can cut through electronic jamming with its electronic couter-counter measure equipment. It has a capacity to carry 50 kg payload. The missile has a height ceiling of 18,000 meters and is capable of detecting and destroying aircraft flying at tree top height. The missile system’s fire control radar is a multi-target and multi-function phased array radar called 'Rajendra' with a range of about 60-km, working in tandem. The radar and the missile can track 64 targets of which four can be engaged simultaneously. The BEL-developed "Rajendra" multi-functional radar system has been integrated with the system. The Akash self propelled launcher (ASPL) and Phased Array Radar have been been developed, though it has yet to enter the production/induction phase. For training the men and officers in handling Akash, scientists have developed simulator of the missile's seeker head in look down role and battery level radar under clutter and jamming environment.

It is a part of the Integrated Guided Missile Development Program (IGMDP) undertaken by the Defence Rasearch Development Organisation (DRDO) in 1983. The system has undergone a few tests earlier to gauge proposition parameters and predicted values. By 1998 five flight trials had been conducted. India's IGMDP was launched in July 1983. Initially, it had a budget of around Rs 400 crore, but it has since been revised Rs 800 crore. The major programs under the IGMDP are the development of missiles including Agni, Prithvi, Akash, Trishul and the Nag. The Sagarika and the Surya have since been added to the IGMDP.



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indian_groom
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«Reply #147 on: April 25, 2006, 10:27:18 PM »
The Trishul (Trident) is a short range, quick reaction, all weather surface-to-air missile designed to counter a low-level attack. It has been flight tested in the sea-skimming role and also against moving targets. It has a range of 9 km and is fitted with a 5.5 kg HE-fragmented warhead. It's detection of target to missile launch is around 6 seconds. The missile can engage targets like aircraft and helicopters, flying between 300 m/s and 500 m/s by using its radar command-to-line-of-sight guidance. It operates in the K-band (20 - 40 GHz), which makes it difficult to jam. In the K-band three-beam system, the missile is initially injected into a wide beam, which then hands it over to a medium beam, which passes over to a narrow beam, guiding it to the target.

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shayar_dildaar
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«Reply #148 on: April 25, 2006, 10:45:26 PM »
Excellent job Desi_Dulhe.....U have done a gr8 job by posting information too..Keep up the effort...[/color][/size]
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indian_groom
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«Reply #149 on: April 26, 2006, 12:35:48 AM »
aur kuch janana ho tau bata dena.....abt defence related...........mujhe
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