THE GANDHIS HAVE THROWN THIS COUNTRY TO DOGS
Arvind Srinivas
Director
Cell : +91-9821784148
arvindsavy@gmail.com
From: govindan menon <tcgmenon@hotmail.com>
To: "indiaresists@lists.riseup.net" <indiaresists@lists.riseup.net>
Sent: Thursday, 14 February 2013 4:09 PM
Subject: [IAC#RG] FW: Copter Deal
To:
---------- Forwarded message ----------
From: Tcg Menon <tcgmenon@gmail.com>
Date: 14 February 2013 14:28
Subject: Copter Deal
To: newsroom@timesnow.com
![AGUSTA HIRUNDO A109.png]()
From: Tcg Menon <tcgmenon@gmail.com>
Date: 14 February 2013 14:28
Subject: Copter Deal
To: newsroom@timesnow.com
Yesterday I watched the debate on 'Times Now' regarding kick-backs in the Helicopter Deal with an Italian Company. Majority of the Retd. Army and Air Force personnel were saying that the original specification might have been altered to ensure more transparency because initially they got only one tender. But it is revealed that there are three countries manufacturing helicopter capable of flying more than 18000 feet high with similar specification and passenger capacity. Details are given below and all the details are available on the internet. The original specification was suitable for evacuation and transportation of military personnel from Kargil and Siachen during the war. Moreover, the original proposal might have been made after Kargil war in 1999. At that time our indigenously- developed Dhruva which can also fly at a height of 20000 feet was not there. The Dhruva entered into service in 2002. So if the Govt. wanted, it could have purchased Dhruva and saved Foreign exchange . Even Israel has purchased Dhruva. Majority of Defence Deal Scams started during Rajiv Gandhi's period, when the Western lobby become powerful and India turned to the West for defence equipments and subsequently scams also increased. By cancelling this Deal , our country 's security will not be jeopardized as we have Dhruva, the production of which should be increased.
T C G
Rajiv Gandhi 1984-1989
Westland helicopter scam
The Prime Minister Rajiv Gandhi forced the public sector Pawan Hans Corporation to buy 21 helicopters from a British company that was shutting down. A series of technical faults and crashes followed. The helicopters were eventually discarded as junk and lined up at an unused airport in Mumbai.
| Tiger hill (highest mountain seen in the background) as seen from the River Indus in Kargil. | |
| 17,411 ft (5,307 m) | |
| Location | |
| Location | |
The Siachen Glacier is located in the eastern Karakoram range in the HimalayaMountains at about 35.421226°N 77.109540°E, just north-east of the point NJ9842where the Line of Control between India and Pakistan ends.[4] At 70 km (43 mi) long, it is the longest glacier in the Karakoram and second-longest in the world's non-polar areas.[5] It falls from an altitude of 5,753 m (18,875 ft) above sea level at its head at Indira Col on the China border down to 3,620 m (11,875 ft) at itsterminus
Agusta A109 Power
Data from www.agustawestland.com[33] [34]
General characteristics
· Crew: 1 or 2 pilots
· Capacity: 7/6 passengers
· Length: 42 ft 9 in (13.04 m)
· Rotor diameter: 36 ft 2 in (11.00 m)
· Height: 11 ft 6 in (3.50 m)
· Powerplant: 2 × Pratt & Whitney Canada 206C or Turbomeca Arrius 2K1turboshafts, 567 hp or 571 hp (423 kW or 426 kW) each
Performance
Data from {Eurocopter EC135 2008 Tech Data book}
· Crew: 1 pilot
· Capacity: up to seven passengers or two crew and two patients (Air Ambulance variant) or 1,455 kg (3,208 lb) payload
· Length: 12.16 m (39 ft 11 in)
· Height: 3.51 m (11 ft 6 in)
· Empty weight: 1,455 kg (3,208 lb)
· Max takeoff weight: 2,910 kg (6,415 lb)
· Powerplant: 2 × Turboméca Arrius 2B2 turboshaft engines, 472 kW (633 hp) each or 2 x Pratt & Whitney Canada PW206B turboshaft engines rated at 463 kW (621 hp) (take-off power)
· Main rotor diameter: 10.2 m (33 ft 6 in)
· Main rotor area: 81.7 m2 (879 sq ft)
Performance
· Cruising speed: 254 km/h (158 mph; 137 kn)
· Range: 635 km (395 mi; 343 nmi)
· Service ceiling: 6,096 m (20,000 ft)
· Rate of climb: 7.62 m/s (1,500 ft/min)
General characteristics.Specifications (Ka-226A)
· Crew: 1
· Passengers: 9
· Cargo: 1,400kg internally, or 1,500kg on an external sling
· Length: 8.1 m (25 ft 7 in)
· Main rotor diameter: 2× 13 m (42 ft 8 in)
· Height: 4.15 m (13 ft 7 in)
· Gross weight: 3400 kg (7496 lb)
· Powerplant: 2 × Turbomeca Arrius 2G1, 335 kW (450 hp) each
Performance
· Maximum speed: 205 km/h (127 mph)
· Cruising speed: 195 km/h (121 mph)
· Range: 600 km (372 miles)
· Service ceiling: 6200 m (20300 ft)
· Hover ceiling: 2500 m (8200 ft)
General characteristics
· Crew: 1 or 2 pilots
· Capacity: 12 passengers (14 passengers with high density seating) or 4 stretchers.
· Length: 15.87 m (52 ft 0.8 in)
· Rotor diameter: 13.20 m (43 ft 3.7 in)
· Height: 4.98 m (16 ft 4.06 in)
· Disc area: 137 m² (1,472 ft²)
· Useful load: 2,600 kg (5,731 lb)
· Powerplant: 2 × Shakti turboshafts, 1,000 kW (1,400 shp[122])
Alternate engine: 2 x Turbomeca TM 333-2B2 turboshaft, 746 kW (1,000 shp) each
Alternate engine: 2 x Turbomeca TM 333-2B2 turboshaft, 746 kW (1,000 shp) each
Performance
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