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Pakistani version of JHMS!!!! On live trial.Any idea about the attachments on the sides of his helmet? Doesn't seem normal.
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Pakistani version of JHMS!!!! On live trial.Any idea about the attachments on the sides of his helmet? Doesn't seem normal.
Just shadows and grey shade nothing special.Any idea about the attachments on the sides of his helmet? Doesn't seem normal.
Hi,
This here is a very interesting video by an F35 pilot. I would like the young pakistanis to listen carefully to what he is saying---.
This video links itself by default of being about an aircraft that was inferior to the current F16 at the time of its inception---I am not talking about the JF17---but the F35---.
This is a gem pf a video.
It then also in-advertantly by default sheds light on the J20 program---as to why the J20 being developed without the right engine---.
Something to keep in mind when discussing LCA/Tejas as well.Hi,
This here is a very interesting video by an F35 pilot. I would like the young pakistanis to listen carefully to what he is saying---.
This video links itself by default of being about an aircraft that was inferior to the current F16 at the time of its inception---I am not talking about the JF17---but the F35---.
This is a gem pf a video.
It then also in-advertantly by default sheds light on the J20 program---as to why the J20 being developed without the right engine---.
Something to keep in mind when discussing LCA/Tejas as well.
@MastanKhan the short answer is that there is no G limit.
G is acceleration of gravity the faster you accelerate the more G you can pull just like the car.
G force is impacted by Configuration of the air craft, Gross weight and attitude of the aircraft and we have to keep in mind the whole airframe is impacted by G and not just the wings.
FCS limits the G on the Jf-17---once override you can literally go to the extent of ripping your wing of and turning your brain in to mush. The structural Limit is more of the JF-17 but it is regulated at +8/-3 this is done because of biology and Increasing air frame life.
Strengthen a single section of the wing will have not a drastic impact on the capability of the G load the wing can handle but might be able to bare more repeated stresses caused by the already rated G for the aircraft.
I am not an aeronautical engineer and nether am I a trained mechanic I just read books and talk to a lot of credible people.
Im glad you had a good laugh.Hi,
You made me laugh at your answer---. Just trying to hold the ear from around the head---hehn.
Im glad you had a good laugh.