What-iffery is fun - but just sometimes it does run up against something, a HISTORICAL " something", that even stopped
the designers and dreamers in their tracks...
OR DID IT???
Look at the Wiki article again -
In 1939, Dornier was busy working on the P.59 high-speed bomber project, which featured the tandem engine layout. In 1940, he commissioned a test aircraft, closely modeled on the airframe of the early versions of the Dornier Do 17 bomber but only 40% of the size of the larger bomber, and fitted with a retractable tricycle landing gear to validate his concept for turning the rear pusher propeller with an engine located far away from it and using a long driveshaft. This aircraft, the Göppingen Gö 9 showed no unforeseen difficulties with this arrangement, but work on the P.59 was stopped in early 1940 when Hermann Göring[citation needed] ordered the cancellation of all projects which would not be completed within a year or so.
But this is NOT the full story!
Look at the Göppingen Gö 9 article!!!
In 1937, Claudius Dornier observed that adding extra engines and propellers to an aircraft in an attempt to increase speed would also attract a penalty of greater drag. He reasoned that this penalty could be minimized by mounting a second propeller at the rear of an aircraft. In order to prevent tail-heaviness, however, the engine would need to be mounted far ahead of it. Dornier patented this idea and commissioned a test plane to evaluate it.
The aircraft was designed by Dr Ulrich Hütter as a 40% sized, scaled-down version of the Dornier Do 17's fuselage and wing panels, and built by Schempp-Hirth. The airframe was entirely of wood, used a retractable tricycle landing gear (one of the earliest German airframe designs to use such an arrangement) with power supplied by a Hirth HM 60 inverted, air-cooled inline four-cylinder engine mounted within the fuselage near the wings. Other than the engine installation, the only other unusual feature of the aircraft was its all-new, full four-surface cruciform tail, which included a large ventral fin/rudder unit of equal area to the dorsal surface. This fin incorporated a small supplementary tailwheel protruding from the ventral fin's lower tip that assisted in keeping the rear-mounted propeller away from the ground during take-off and landing. The Gö 9 carried the civil registration D-EBYW.
Initially towed aloft, flight tests began in June 1941...
They went on with the project privately!!!
...but later flights operated under its own power. The design validated Dornier's ideas, and he went ahead with his original plan to build a high-performance aircraft with propellers at the front and rear, producing the Dornier Do 335.
It looks like only
Heerswaffenampt FUNDING was perhaps halted!
So here's the rub...
1937 to 1941+ is
five years;
before Dornier could go ahead with the Do 335 "
Projekt P.231" there was FIVE YEARS of design work, testing and concept testing
I wouldn't like to guess how much design time WASN'T actually lost by the simple withdrawal of government funding! That being the case -
COULD work on the historical P.231/Do335 have progressed any faster than OTL??? Claude Dornier was making pots of dosh from his aircraft factories, he could fund his
own design work and concept testing!

And obviously
DID....
I don't think your particular POD is going to buy back as much time ATL for the DO 335 entering service as you think....

Twenty years ago we had Johnny Cash, Bob Hope and Steve Jobs. Now we have no Cash, no Hope and no Jobs....
Lord, please keep Kevin Bacon alive...