Quote:
Originally Posted by Crumpp
They did rush it!!'
If we take January 1942 as the time the conversion for Spitfire Mk I's was complete that represents about two years and four months between initial flight test and 100% ground operational adoption.
Compare that to the RLM's testing of 1.58ata/1.65 ata as a straight manifold pressure increase in the BMW801D2. The motor was tested at that manifold pressure in May 1942. It was not until July 1944 that we see it in the Flugzueg Handbuch for the FW-190A8. That is a two years and two months lag time. Do you not think the RLM was rushing this improvement, too?
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Now you are an expert on processes in engineering companies. Who'd have thunk it
Quote:
Originally Posted by Glider
What is your training and background?
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He's been an "Advisor to the Experts" for several years now.