Originally posted by Kev367th
No you read this -
"[...]In September 1944 an equipment kit was installed which raised boost pressure and increased the Jumo 213 A's emergency output from 1,750 to 1,900 h.p. The installation was carried out on-site by Junker's Tecnical Field Service (TAM). This increased emergency power could be used at altitudes to 5000 meters. At the same time, use of takeoff power (1,750 h.p.) was extended to 30 min., while authorization was given to use combat power (1,620 h.p.) without restriction. "
1900hp was possible on ata1.7 - this is the increased performance mod referred to in your
By the end of December 1944 there were 183 Fw 190's in operation with the increased performance modification, and 60 more had been delivered with the MW 50 system and were at the point of entering service.
It is NOT the MW-50 and ata1.8 modification.
Let me simplify -
183 Fw-190D9 with the 1st mod by end Dec 1944, 60 with the MW-50 ata1.8 modifcation ABOUT TO ENTER SERVICE by the end of Dec 1944.
You can 'fudge' all you want with dates, but they were still trialling/testing 1.8ata in October 1944.
It was starting to be fitted to production aircraft November 1944
Deliveries to units began end December 1944.
Yup you are right, I had to dig out Dietmar Hermann's book to make sure the quotes weren't mixed up...
Climb & Combat 1620 PS ~ 1,4 ata
Take-off/Emergency 1750 PS ~ 1,5 ata
Increased Emergency 1900 PS ~ 1,7 ata
MW50 injection 2100PS ~ 1,78 ata
But we only talking about a few of months here (Jan '45 rather then Sept '44) and only for WEP at that (10 min on 5 off in AH). If you read MWs site at 1.7 ata / 1900 PS you gain 10 - 11 mph below full throttle height take-off power (above 1750 PS)and gain 20 - 22 mph with MW-50 (1.78 ata 2100 PS) above 1750 PS.
Based on the flight results, and allowing for variations, it can be stated that a gain in speed of 10 to 11 mph (16 to 18 km/h) is obtained below full throttle height using take-off power increased to 1900 PS. 20 ½ to 21 ¾ mph (33 to 35 km/h) can be obtained using MW 50 installation, with the 160 Ltr. - nozzle.
and
The enclosed speed graph shows level flight performance with Increased Take-off power (1900 HP - basis) and Special- Emergency power. As evident, a gain in speed of 13 to 15 km/h is obtained by the gap sealing. Level speeds at Sea Level:
According to Naudet:
And to give a quick glance on the MW50 test, Wk.-Nr. 210 002 reached speeds of 570-580 km/h with Erhoehte Notleitung and 590-595km/h at SL using MW50, without ETC504 attached and a puttied and polished surface.
In a later test were a gap between engine and wing was covered, 002 managed 608km/h at SL using MW50.
But all tests were done using underperforming engines, mentioned in both FW and Junkers documents and so they approve Hennings oppion that the engine of 002 was somewhat "bad". He was right, because the first serial production chargers did not reach intended full boost altitude and airflow, according to Junkers reports of benchtests with there JUMO213 engines from the first serial production batch.
And funny to note, comparative test with Wk.-Nr. 210 001 with standard factory surface finish reached the same speeds as 002. FW was a bit curious why the higher quality surface finish of 002 did not show in better performance and were keen to investigate that issue further.
The conclusion of FW was that with engines performing to the published figures and good factory finish a serial production D9 will reach the calculated performance figures.
According Whels last test on AH deck speeds the AH D-9 does
190D-9 346 mph (557 km/h) MIL
190D-9 375 mph (604 km/h) WEP compared to 378 mph (608 km/h) MW-50
If this is still true the AH2s D-9 may match up well with a Jan '45 D-9 running at max 1.78 / 1.80 ata 2100 PS and should be adjusted to reflect that. However, someone should run full tests to be sure.
here's what Butch said:
The Oldenburg Gerät was indeed an MW-50 system which was not mounted on every airframe, it was based on an MW-50 tank not the dual MW-50/fuel tank which was used on the later serialized system (beginning february 1945).
The Oldenburg Gerät (LP MW-50 system) were installed during production in the early part of November '44 and III./JG54 received 60 by the end of December.
FYI
PS is the metric equivalent of HP (2100 PS = 2071 HP / 1900 PS = 1874 HP) on MW's site HP / PS are inter mixed.