Vasily Zaytsev
FULL MEMBER
- Joined
- Jan 24, 2010
- Messages
- 645
- Reaction score
- 0
Ooops! You seem to be all mixed up!
The Israeli EXTRA shown above. Since the IDF had decided to forego the LORA in favour of
the EXTRA, the Indian Army too decided in favour of the EXTRA's design/performance
parameters. Subsequently, a military-industrial cooperation plan was put into effect for producing the
EXTRA in India with 'Indian characteristics', and rechristened PRAHAAR.
The solid-fueled Prahaar surface-to-surface battlefield support missile, is destined to replace about 350-odd existing Prithvi SS-150 liquid-fuelled battlefield interdiction missiles that are now nearing the end of their service lives. The Prahaar will come packed in a six-unit pod configuration on board a high-mobility BEML-TATRA wheeled vehicle housing both a SATCOM-equipped command-and-control shelter as well as a transporter-erector-launcher mechanism designed by Larsen & Toubro.
The Prahar follows a relatively simple three-element design, comprising a warhead in the fore section, propulsion unit, including the solid-fuel rocket motor with a nozzle. The nozzle is encircled by the navigation, flight control and guidance unit, which includes the integrated avionic guidance and flight control section, cruciform tail control surfaces, actuators, related antennas and connectors. The Prahaar can be launched within few minutes, from unprepared positions. In fact, any target whose location is known within the range of the missile can be attacked within less than 10 minutes from the launch decision. Each Prahaar will be housed within a disposable sealed cannister providing a 10-year service-life and very low maintenance costs. The Prahaar will have a range of 150km and carry a 125kg (275lb) warhead.
Launch weight will be about 430kg (990lb), and CEP will be well within 10 metres. Equipped with a fibre-optic gyro-based inertial navigation system combined with a GPS receiver, the Prahaar will use an aft section fitted with stabilising fins and a solid-rocket motor. The warhead section will be built as a modular compartment, designed to carry various types of sub-munitions or a unitary warhead. For example, it will be able to carry up to 400 AT/AP bomblets, scatterable mines, anti-runway munitions and similar loads. The fin-mounted control section will store the guidance and control avionics, driving four flight control surfaces for trajectory shaping.
ThePrahaar has been developed by the DRDO in cooperation with Israel Aircraft Industries (IAI) MLM Systems Integration Division and Israel Military Industries (IMI) Rocket Systems Division as a modular kit.
So there! The Prahaar has nothing in common with the AAD architecture.
Cheers!
Don't post Rubbish you nutcase.
You seem to be the second avatar of Chorgupta.
Point any parameter of EXTRA that is identical with Prahaar,
Before posting read what are you posting.
Please put your head out from the place where the sun does not shine.