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I thought the structural failures mentioned were caused by the inferior glue, used on the aircraft. Hardly suprising IMO look at the time in which it was build, late in WWII.
Below a picture I took of a salamander at Hendon RAF museum. It really is a beautiful a/c
The landing gear door and alieron failure were caused by faulty glue. I think the rudder failures were due to overstressing the aircraft.
Most everything I heard about this fighter was positive, particularly considering how fast it went from first pencil on drawing to flight test.
IIRC it didn't actually go into an Operational squadron until late March, early April? but was in production in December 1944. If my memory serves me, what were the key milestones that it needed to pass before deployment?
Was JG 1 or 2 the first operational unit?
The difference between the 162 and other combat aircraft was it was designed so it could be flown by HJ who had some time in gliders. Very low hour pilots indeed.
Eric Brown believed this bit was a joke as no novice was going to fly the 162 safely.
So the 162 did not meet its design brief.
The short range of the 162 meant it could only be used for point defence of its own airfield.
I understand your point but the question is whether the 162 would have entered service in the RAF or USAAC...I think not.
I doubt they would have accepted it.
Even if the 162 could go at the bombers it was no use in the ground attack role.and the Germans needed a good one of those too.
The 162 took away resources that may have been better spent on the Ar 234 or Me 262.
It isn't often Soren and I are in total agreement but we are in this case. Eric Brown was probably unique at this time as he had flown all the jets then flying, German, American and British and this was the one he liked the most.
Re the rudder being overly sensitive, no doubt if the German designers had a little more time, this would have been resolved in the normal process of moving an aircraft from prototype to production. Its what test flying is designed to do.