Thrust to Weight(ratio) of 11?
For reference, the T/W of F119 is ~9.00, and F135 is ~11.47.Yup.
Did they mentioned anything about the maximum (afterburning) thrust of WS-15?
Thrust to Weight(ratio) of 11?
For reference, the T/W of F119 is ~9.00, and F135 is ~11.47.Yup.
No real spec details on the WS-15.For reference, the T/W of F119 is 9, and F135 is 11.47.
Did they mentioned anything about the maximum thrust of WS-15?
Old rumor from maybe the late 2000s early 2010s.Do you know where this rumor/claim (WS-15 based on R-79) comes from? I don't remember it.
not talking about technical details.For reference, the T/W of F119 is ~9.00, and F135 is ~11.47.
Did they mentioned anything about the maximum (afterburning) thrust of WS-15?
Still trying to square how 110 kN military thrust at a bypass ratio of 0.25 translates to a wet thrust of 180 kN.not talking about technical details.
but WS-15 stands in between F-119 and F-135 if we talk about general specifications. like T/W and total thrust
huge accomplishment for China.
we should wait for official details.Still trying to square how 110 kN military thrust at a bypass ratio of 0.25 translates to a wet thrust of 180 kN.
Some EW can be done by plugging in the cord.No, EW can absolutely be done by one crew member, it's just that the requirements for what constitutes "EW" in one age versus another, and in terms of the expectations for the host aircraft to survive XYZ combat environment or XYZ distance from enemy, is different.
It is so - precisely that second dedicated person for specific demands.If the PLA do go for the twin seat J-20, it's not because a single seat J-20 can't do EW (or for that matter, drone command), but because they want a twin seat J-20 with a second human being that can do all of it even better than a single seater can in more demanding environments.
Some EW can be done by plugging in the cord.
Some still requires whole rows of operators, every single of which has maybe dozen or two of comparable colleagues around the world.
Dedicated operator needs and will continue to need operator(s), fully dedicated to it and not busy with flight-related tasks.
Erm, this is a very bad example, because the lack of EF-111 replacement (now rushed in EW form of F-15EX) is currently seen as a core deficit of USAF structure, and EA-6 was directly replaced by F-18G(also with complaints that it isn't enough for deck use, since there is no guarantee larger USAF EW assets will be there to back it up).Heck, the nature of technology means that contemporary aircraft with a single pilot can do EW in a more capable manner than dedicated multi crew EW aircraft from years past. (Think F-35 compared to EF-111 or EA-6)
I personally think that the current J-20, as it is, is absolutely disastrous as a dedicated EW platform. It won't escort anything, it won't be able to degrade opponents' SA picture, comms, anything.What this means for J-20 in the EW role, is that I expect a single seat J-20 to be absolutely highly capable as a EW platform and able to effectively operate in that role. However I expect a twin seat J-20 to be more capable as a EW platform and operate more effectively in that role.
The side weaponsbays can be repurposed to carry EW arrays for flanking jamming/ELINT.is absolutely disastrous as a dedicated EW platform.