I do agree that we should have better data available, re. weight of the DB-Falke, in order to do some estimates. The P-38J weighted 17000 lbs (~7720 kg )with full ammo and internal fuel, no drop tanks. The Falke was slightly smaller and was not carrying turbos, so it would be reasonable to estimate the weight of the DB-601 version at 6000 kg, loaded, clean?We have a problem with the "modest" weight. The Jumo powered versions went 4900-5000kg clean. No argument there. We have no weight figures for a BD 601 powered version. The data for the proposed DB 605 powered version has a weight of 7200KG clean and a proposed high altitude variant with single seat and two 20mm MG 151s and two MG 131s was 6000kg.
The next question is what kind of fields are being used. Using a P-38L as an example (because I could get the chart easy) which is both heavier and has more power the take off distance changes by 300 ft on a hard runway with an increase of 2000lbs but changes by 500 ft on a soft runway. That is at 32 degrees F, add 10% for every 20 degrees F above freezing. take off on soft runway at 60 degrees F at 19,400lbs (middle line on the chart) is almost 2400ft. take off on hard runway at 17,400lbs is 1300ft at same temp.
FWIW, the P-38F was able to take off with two dummy torpedoes - 3500 lbs worth?
The early DB engines are no more a high altitude engine than a 1940-41 Allison was. Was gives the early DB engine the reputation of a high altitude engine was that it was installed in a 2700-3000 KG fighter instead of a 3400-3600kg fighter. IF the DB 601N powered fighter weighs 5600 kg it will have the same power to weight ratio as a 109F-2 with a slightly higher wing loading. Using DB 601A type engines even if the plane is several hundred KG lighter doesn't improve things.
I was not referring to the 601A as a high altitude engine, and certainly don't agree with such reputation if it exists. I was referring to Steve's estimate: "High altitude interceptor?......Possibly with substantial modification." - installation of newer versions of the DB-601/605 engines as they become available does not require substantial modifications of the basic airframe stressed for the DB-601A.
SAVING money buy building "lighter" Fw 187s (There is only about 1600lbs difference in empty weight between a Jumo powered FW 187 and a Bf 110C wigh DB 601s) kind of goes out the window when you replace the 11,220lb empty weight Bf 110G night fighter with a 19,973lb empty Ju 88C night fighter. While cost to build is not directly linked to airframe weight is was close enough that it was used for many 'quick' comparisons.
You can see in the post you've quoted that Me-210 saga is very unlikely to happen, that means also the Me-410 is deleted. Further savings are due to the less losses of the better performer (DB Falke vs. Bf-110), LW and RA loses less bombers when attacking Malta and Med convoys, LW looses less (far less?) Ju-52s while trying to reinforce Afica Corps due to the escort provided. Less LW bombers lost means the losses in crews are smaller, while the damage inflicted to the Allies is greater. During Op Pedestal, RN loses two CVs (instead of one); tanker Ohio does not make it to Malta?
The number of engines for Ju-88 instead of Me-210 night fighters remains the same, as well as number of electronics sets required, so the price per night fighter produced should be just a tad greater.