Alok Arya
FULL MEMBER
New Recruit
- Joined
- Jan 25, 2017
- Messages
- 50
- Reaction score
- -1
- Country
- Location
Yes sir non quad fbw is more tiring , more attentive , pilot has less time to focus no weapon system . Also non quad fbw usually used in plane which are non rss .This is the first time I saw arguments like "Tejas is less tiring" and "IFR probe is useless because the pilot is too tired".
Normally I don't reply to ridiculous arguments like these, but the shock value from your post alone is worth replying to.
Alright, what's first.
Literally all the news articles about what the block 2 upgrade is will tell you there is a upgrade to avionics. And it's on JF-17's wikipedia page. If it's too inauthentic to you, I'm sure plently in the JF-17 section of this forum would be willing to tell you. I'm too tired to be looking for a link from my phone at 5AM in the morning.
Also, since you asked me to support my claim. Please support your claims of "flying a quad fbw plane is hand free job and flying a plane with out same is too tiring(by the way do you even know what redundancy is for?)" and "is of no value as pilot is already exhausted". With "authentic link", of course. And the standard of the link's authenticity is ambiguous that is deemed by me.
What makes you think that JF-17 pilot would be tired just after 45 minutes of flying? This is not WWII, when you have to change the trim, fuel mixture, propeller pitch constantly just to maintain a level flight. Even the early JF-17 with pitch only FBW had stability control for yaw and roll. The plane would happily maintain its attitude by itself.
Assuming "Non-quad-redundant FBW makes pilot tired, so tired that they can't complete a IFR after 45 minutes." is true.(Which it isn't.)
Be sure to tell that to designers of early planes with IFR probe but not FBW, that "it is of cosmetic value". They don't even have FBW, IFR probes must be for less than cosmetic value!
Alright, I accept this explaination. So they wasted their opportunity on saving weight by have a massive wing then? Okay. Hope the lower wing loading is worth it.
But I wonder where this "which is going to reduced for Tejas" comes from. If you look at pretty much ALL historical plane developments, they only get heavier.
Really, find a Tejas vs Thunder argument. ANYWHERE. I guarantee that the word "composite" will be mentioned.
We are comparing planes here, not budget or training. Stay on topic would ya.
I believe my English is not good enough to comprehend this argument.
You are right block 2 has lot of improvement in avionics . But fbw is not avionics . It is basic aircraft system . I am not not saying that future version of jf 17 may not have quad fbw . There can be very well quad in future version, but at present there is no authentic new of quad fbw in block 2 or 3 . So it is not present only assumption are there .
Wing area is degine parameter . Tejas wing give Tejas high agility , lower wing loading , true vortex effect negating need of canard , and these are all parameter from where Tejas edge jf 17 in basic degine with superior performance however it is very slight according to you . But I appreciate you to give us slight edge .
Weight saving will come from HAL work on lca navy with redegining of landing gear and some over engineered part , removal of ballast in nose cone , and use of better composite . But you are again true that developmental history of planes mark by weight gain due to avionics . And this is the case for both Tejas and jf 17 , both will go heavier with future addition of avionics so some of Tejas weight reduction will be negated by weight gain because of avionics .
I know that fighter no is increasing with time , so is flight hour , that is why I give flight hour in range , from 10 to 20,000 hr total .You are dense mate, with PAC producing some 16 aircraft per year and current strength of around 80 JF-17s, how is it possible that PAF had 70 Thunders for the last five years......easy maths.