Well, both 400 and 500 I am laking.
to ask Stealth Spy, Where is he now?
Unlikely. The B-1B hasd a much more extensive use of RAM, is smaller, more blended, less visible engine faces, a fixed inclined phased array antenna, and a coated windscreen.
This only for B-1A I think
I have seen a video/article somewhere where the frontal engines and naclles on the TU-160 were coated in RAM.
Where?:eek:
http://www.youtube.com/watch?v=Uz5gCUC7vZM
Google is your friend. seriously theres loads of vids out there, that took me all of 15 secs to find, maybe just 10 🙂
You must be joking. I just saw a SHE fly by, not a demonstration, do you have any complete edition?:p
I’m not 100% sure, but I think I already saw E models during demos. But I guess the F makes more sense, as you can take a crew member along.
I recall reading many years ago, that the Turkish air force preferred the two-seat F-5B over the single-seat F-5A for its air display team – it just had better flying qualities for the role.
Perhaps it’s got something to do with weight and Centre of Gravity considerations?:confused:
What? Call me idiot if you can give me the link show those demonstration in air show done by E version of SH to me.
I am sure I never find it in youtube.:(
I always considered that J-8II is something imitated from Su-15.
The target is 1:12 (engine-weight to AB-thrust), when 1:10 is the baseline to start from. There are some tricks to “fine-tune” that, when it comes to weight of engine. Related to choosen “engine-weight” that ratio can differ from 1:10 till 1:11.
It won’t be late when it actually get 12:1 T/W rate.:D
How much thrust does the F-135 make?
That’s your problem not mine
The F-15 was designed in the 60s and the AAMs had still to mature.
Compare that to the F-15E of the 80s and you will learn the difference.
The weight issue is limited to the F-35B in general.
The F-22 is overweight by some thousand lbs at all.
That’s it! So Just compare weight is meaningless. Relating with 78 ms wing area of F-22, overweight thousands lbs also is acceptable, but for F-35 it must be a disaster
If the engine that will fit on F-35 can make thrust over 20ton, I won’t worry it any more.
How smart you are! Escape from keypoint and pick up plausibility.
Yes, weight is carried by lift, keypoint here is that empty weight should be as smaller as possible. When F-15 take the weight lighter enough, we saw American said we cut each grams if it is possible, when F-35 overweight, we see an allegation of ignoring the weight problem.
Most of standard made by US, they will pick any one from which they benefit.:rolleyes:
Oh, please…….the weight of the Flanker Series. Is vastly more than most of its contemporaries. Yet, does anyone here consider it to be a poor dogfighter!:p
The weight seriously concerning to TW rate. We are not here going to compare with weight. Most of jets has already been heavier then warplane in WW2. Nobody said flight performance of jets are poorer than propeller, but velocity of power and weight still is top important.
This is the reason why Boeing lost JSF program. They are good at creating new glossary more than do something practically.
What does 4.75 generation mean? jeu de mots? :diablo:
If my memory is right, the flight envelop of tornado is drawn by a russia web? Who remember that link?
That Mirage 4000 can load 10 missiles with a external fuel tank under center line simultaniously, what if F-16XL performence a2a mission?
many aircraft can do supersonic without reheating, the key is value. less than Mach 1.4 won’t be super cruise.
Aarh…. Super….. again!
Now each thing made in USA got super prefix for any purpose……:D
Please take care, have you painted some gold on these many super, don’t you think it will ressemble to inflated curruncy?
May I down-grate the F-22 to third generation since many 3nd jet has up-grated to have super-cruise even more super*** brabra…..:p