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Re: IAF to buy 14 Tejas squadrons
give me TWR figues in KN with weight and thrust of two engines.
http://defenceforumindia.com/thrust-to-weight-ratio-fighter-plane-460
It is given as 0.69 for jag.
It gives a TWR of 0.87 for tejas by taking 3.5 ton fuel as limit!!!!
the internal fuel of tejas is just 3 tons, So how can one measure it with 3.5 ton fuel is a mystery.
but if we take the half fuel weight along with empty weight the TWr of tejas comes to 1.07 .
What will it come to jag/
Empty weight - 7 tons,
half fuel -1.5 tons,
http://honeywell.com/News/Pages/02.10.09JaguarFighterAircraft.aspx
this source says it has a wet thrust of 44 Kn each in each engine meaning 88 Kn,
So with new honey well engine if the figures are correct it gets a TWR of around 1 close to tejas figure.
i took the figure mentioned in the old link above,
But how much of this thrust can be used by the very old airframe design to improve its performance in turns yet to be certified.
http://en.wikipedia.org/wiki/SEPECAT_Jaguar
This link gives the total wet thrust of two engines as 65 Kn at present.
So at present it is supposed to have a TWR of 0.76.
3505 kg = 7727 lb@ersakthivel
jaguar t/w of 0.64 ? with honeywell F125IN with 6230 lbf dry thrust ???
give me TWR figues in KN with weight and thrust of two engines.
http://defenceforumindia.com/thrust-to-weight-ratio-fighter-plane-460
It is given as 0.69 for jag.
It gives a TWR of 0.87 for tejas by taking 3.5 ton fuel as limit!!!!
the internal fuel of tejas is just 3 tons, So how can one measure it with 3.5 ton fuel is a mystery.
but if we take the half fuel weight along with empty weight the TWr of tejas comes to 1.07 .
What will it come to jag/
Empty weight - 7 tons,
half fuel -1.5 tons,
http://honeywell.com/News/Pages/02.10.09JaguarFighterAircraft.aspx
this source says it has a wet thrust of 44 Kn each in each engine meaning 88 Kn,
So with new honey well engine if the figures are correct it gets a TWR of around 1 close to tejas figure.
i took the figure mentioned in the old link above,
But how much of this thrust can be used by the very old airframe design to improve its performance in turns yet to be certified.
http://en.wikipedia.org/wiki/SEPECAT_Jaguar
This link gives the total wet thrust of two engines as 65 Kn at present.
So at present it is supposed to have a TWR of 0.76.
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