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*the 'Monografie Lotnize' book states that Ta-152H-0 did not featured GM-1 nor MW-50 tanks, the rear tank being filled with 115L of fuel instead. The H-1 was to have 85L of GM-1 mixture (tank in rear fuselage) and 70L of MW-50.That sounds right to me. Hermann reckons that the H-1 and H-10 should both have had both systems as standard.
Cheers
Steve
That defies common sense. P-38J didn't enter service until August 1943. P-38H and earlier models carried less fuel then Fw-187 and the aircraft was considerably heavier. How could P-38H possibly have twice the range?
Me309 had an approximate range of 685 miles (1,100 km) which was just a few miles further than the Fw187, neither of which could compare to the P-38's range of about 1,300 miles
That defies common sense. P-38J didn't enter service until August 1943. P-38H and earlier models carried less fuel then Fw-187 and the aircraft was considerably heavier. How could P-38H possibly have twice the range?
If we were to believe the books as new as from yaer 2008 (4+Publication book on the Ta-152), the BMW-801D in the Fw-190 was featuring a two stage supercharger??The same book says this about the Jumo-213:
It must be stressed that this engine was not turbo-supercharged (ie., it did not have supercharging from the recycling of hot exhaust gases, but used instead air).
Used the air to power the supercharging??
The same book hardly mentions that Jumo 213E was a better hi-alt engine because it was outfitted with a 2-stage supercharger, and we cannot read that DB-603L was featuring the same. On the other hand, the MW-50 and GM-1 abbreviations are mentioned in almost every second sentence, despite the Ta-152H-0 being without those.
What were the main disappointments?
*the 'Monografie Lotnize' book states that Ta-152H-0 did not featured GM-1 nor MW-50 tanks, the rear tank being filled with 115L of fuel instead. The H-1 was to have 85L of GM-1 mixture (tank in rear fuselage) and 70L of MW-50.That sounds right to me. Hermann reckons that the H-1 and H-10 should both have had both systems as standard.
Cheers
Steve
That's my understanding, too, with the MW-50 being in the left inside (nearest the wing root) bag tank and the GM-1 being in the tank behind the cockpit. Also, I don't believe that the H-0 had the wing tanks; only the H-1. But as usual I could be wrong.
Hi, Silence. Sorry if I was not being crystal clear.
The D-12 and D-13 were to be equipped with 4 wing tanks each, exact volume is unknown to me. The volume of fuel in wing tanks of the Ta-152H-1* was 400L in five tanks, the 6th tank (inner left actually; noted at drawing, too) was to carry 70L of MW-50, so that would yield some 330L for the Doras with wing tanks? The position for the 2 wing tanks was to serve as a place for verically-fired weapons, tanks not being installed in that case.
Hope that I'm not mistaking about following:
The Fw-152C-1 and 152E-1 were to carry fuel in all 6 tanks, 1064L total (vs. 994L for the 152H-1), the C-1 and E-1 tanks for MW-50 being in rear fuselage (140L for those two) . Here is the fuel and MW-50 volume listed.
I'm not familiar with /R11 nor /R16 equipment sets, care to elaborate?
Between the wing stations (ribs?) 3 and 4, and 7 and 9 the late Doras were to carry tanks, the Ta-152 was to carry another between the stations (ribs?) 4 and 6.
*the 'Monografie Lotnize' book states that Ta-152H-0 did not featured GM-1 nor MW-50 tanks, the rear tank being filled with 115L of fuel instead. The H-1 was to have 85L of GM-1 mixture (tank in rear fuselage) and 70L of MW-50.
View attachment 247651
I asked myself, that a while back, GregWhat has all this to do with the Do 335, the title of this thread?
Just saying ...