GregP
Major
Original Dornier flight test footage ... seems pretty interesting to me. Enjoy!
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That is a big plane!
A very advanced aircraft. It had hydraulically boosted controls surfaces. It also had a significant sized bomb bay. The rear propellor and upper vertical fin could be blown off at the roots through hollow and explosive bolts for a bailout. It had a compressed air ejection seat. The lower fin could be jettisoned in case of a belly landing. They developed a microwave radar that fitted into the wing leading edges, CIOS made a report on it. I have a speed chart showing the anticipated speed with the DB603L engine was 495mph. The even more powerful DB603M (2800hp) was around the corner as well.
The Ta 152, Do 335 and Ju 388 were the last 3 piston engined aircraft on scheduled for production by the 3rd Reich. They wanted an all jet force but for certain missions piston engined aircraft were still neccesary.
There were projected versions with a jet engine replacing the rear piston engine, versions with the 3000hp Jumo 222E/F and a laminar wing.
The push/pull configuration seems to have been superior to two separate engines in the wing.
Germany would have been much better served investing the effort in a conventional design. Something like a Hornet was well within their capability.
There were projected versions with a jet engine replacing the rear piston engine, versions with the 3000hp Jumo 222E/F and a laminar wing.
The push/pull configuration seems to have been superior to two separate engines in the wing.
The waste of time and resources becomes even clearer when you compare the Do 335 to its conventionally-laid out contemporaries, the de Havilland Hornet and the Grumman F7F Tigercat. The unconventional design lead an aircraft with very much the same performance and warload characteristics (about 470 mph, 4 cannons, 2000 lb bombload), with a far worse cockpit view, cooling difficulties, and highly problematic emergency exit. Not to mention how the much greater polar moment must have lead to decreased manoueverability.
Germany would have been much better served investing the effort in a conventional design. Something like a Hornet was well within their capability.
The Do 335 with DB603LA engine (87 octane plus MW50 circa 2200hp) could get 790kmh, that's 490mph..
Beyond that we're the DB603LM (2400hp, with C3 plus MW50) and beyond that the DB603N (2800hp via RPM). A simple cube law suggests speeds of well over 505 mph to 525 for the DB603N.
Was that flown? In the graph there are multiple markers for 603A, AS and E test flight results but none for the LA. And was the speeds with or without compressibility correction?
IMHO at those speeds one got overly optimistic figures with simple cube law calculations because of fast drag rise and decreasing propeller effectiveness. And how many 603Ns were tested?
There must be a reason Dornier went for a push, pull configuration. Such decisions would not have been taken flippantly by uninformed, inexperienced men.