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Well I am talking about the ratio. 1500/1000 kg i.e. 2/3. Its absolutely impossible. Usually ratio is 1/4 - 1/3:You are talking about the old one, with the one engine.
Adcom Unveils Innovative UAV at Dubai Air Show
Dubai Air Show
by David Donald
November 13, 2011, 10:58 AM
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Yabhon-Namrod UAV Warhead
Displayed alongside the United 40 is a new weapon intended for use with the UAV. The Yabhon-Namrod has been designed by Adcom to be carried internally on an eight-round rotary launcher. It has a straight wing that swivels into position on launch, and a small jet engine that can power the weapon to around 620 mph over a range of around 37 miles.
Yabhon-Namrod weighs about 66 pounds. The warhead is based on that of a standard 100mm artillery round. A range of guidance methods could be employed, including infrared and laser, as well as GPS/inertial.
AINonline
United 40 goes twin
By: Published: 19 Feb 2013
…
United 40 can carry up to 10 powered precision bombs, with four carried externally on pylons under the rear wing, and six more on an internal launcher.
The weapons have a swivelling wing and a small jet engine.
Janes.com
Well concept is interesting. Originally it supposed to have one push propeller with hybrid engine. Now they switched to two regular engines with two propellers. That's less effecient than one. I doubt it will fly for 100 hours and 1000 kg of load for this size UAV is obviously way overstretched.
Well I am talking about the ratio. 1500/1000 kg i.e. 2/3. Its absolutely impossible. Usually ratio is 1/4 - 1/3:
Heron-1 - 1,150/250 kg
Heron TP - 4,650/1,000 kg
Hermes 450 - 550/180 kg
Reaper - 4,760/1,700 kg
Grey Eagle - 1,633/360 kg
Predator - 1,020/340 kg
Its you who cant understand that no UAV in the world has 2/3 payload/max take off ratio.I dont unduerstand why this is rocket science to u, it simple
this is a standard calculation for all UAV
Max takeoff = empty weight+payload weight
Its you who cant understand that no UAV in the world has 2/3 payload/max take off ratio.
Max takeoff = empty weight+payload weight+fuel.