DRDO RUSTOM PDF
PUNE: The Defence Research and Development Organisation (DRDO) on Friday said the Rustom-2 drone would be ready for use in two years. India’s Defence Research and Development Organisation (DRDO) conducted the first flight of a prototype of Rustom-II (Tapas ) medium-altitude. India’s Defence Research and Development Organisation successfully completed the test flight of its Rustom 2 drone at the Aeronautical Test.
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The necessity for local drone production is an urgent one since the state is battling terrorist groups and threats from within and without. Ruetom International Industry Multimedia. This entry’s maximum listed speed mph. This will alert our moderators to take action Name Reason for reporting: Electronic warfare Samyukta Tarang.
Defence Research and Development Organisation.
Many countries today are pursuing their own indigenous drone programs with mixed results. Will be displayed Will not be displayed Will be displayed. Helina BrahMos Air launched Variant. Your Reason has been Reported to the admin. As of this writing Decemberthe Rustom is in active development. The Rustom features a maximum speed value of miles per hour with a range out to miles Rustom-I and Rustom-H. Despite being one of the largest if not THE largest customer of military purchases in the world, the Indian military-industrial complex has been hard at work at developing internal solutions to promote a more self-reliant Indian military inventory.
It completed its 8th successful flight on 8 Dec More trouble roiled the Rustom II program in when lack of access to critical components, like engines and sensors, delayed its flight testing. The Rustom II uses tricycle pattern retractable landing gear, although the frontal gear appears inconveniently close to the FLIR camera. Fill in your details: Get instant notifications from Economic Times Allow Not now You can switch off notifications anytime using browser settings.
The payload limit is listed at lbs while the empty airframe weighs 1,lbs. Mahalingam Keshav Dattatreya Nayak. From Wikipedia, the free encyclopedia. Retrieved from ” https: Post was not sent – check your email addresses! Find this comment offensive?
What is Rustom 2 drone?
Archived from the original on 5 June Sincehowever, a heavier model called the Rustom II was being groomed for an offensive role. With two horsepower engines—sources claim Russian or European origin—the Rustom II soars to a maximum ceiling of 35, feet, with mission altitude at 40, ft.
It sports a three-legged, fixed undercarriage, rear-mounted main wing appendages and a canard wing assembly at front. February – The Rustom-2 product was successfully flown in a production-quality form on February 25th. At present, the Rustom II has just finished its pre-flight trials in early The test was conducted in Hosur.
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Stated by the DRDO, the taxiing and takeoff was exactly as planned. Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Unmanned aerial vehicle UAV.
India’s Home-Made Drone ‘Rustom 2’ Flies With High-Power Engine
Sorry, your blog cannot share posts by email. This will alert our moderators to take action. The second “maiden” flight took place on 15 Oct Relative Maximum Speed Rating. Foul language Slanderous Inciting hatred against a certain community Others.
Never miss a great news story! Power is served through an American Lycoming O series 4-cylinder engine of horsepower. Outwardly, the Rustom rusttom shares an appearance not unlike a Burt Rutan light aircraft design.
Tejas Advanced Medium Combat Aircraft. The Rustom-H shares a wholly different physical configuration than the Rustom-I prototype as it sports mid-set, straight main wing appendages, a bulbous nose section ala the Northrop Grumman Global Hawka retractable, three-legged undercarriage and a tapering empennage. Akash Trishul Maitri missile Barak 8.
The Rustom-I will feature a contained ddrdo endurance window of 12 hours while the Rustom-H is said to double that value as well as fly at higher altitudes. Vertical fins are set at the main wing tips. The powerplant is contained in the aft section of the fuselage driving a two-bladed propeller in a “pusher” configuration. This flight assumes significance due to the fact that this is the first flight in user configuration with higher power engine,” a statement read. It is capable of carrying different combination of payloads including synthetic aperture radar, electronic intelligence systems and situational awareness systems.
This was the first flight of the UAV in user configuration with higher power engine. This page was last edited on 19 Septemberat