I would really like to see the figures that will convincingly show that the Fw-187 would have done all of these things, particularly the climbing and diving: I have Hermann and Petrick's book on the Fw 187 and all I see are lots of projected performance figures for planned Fw 187 derivatives when fitted with various engine types, including the DB605. There is no mention anywhere of the confirmed or projected diving speeds so I cannot see how such claims can be confirmed.
Fw 187 V4 rate of climb = 12.1 m/sec = 2,381 ft/min, gross weight = 4,900 kg: projected Fw 187 with DB605 = 13 m/sec = 2,559 ft/min, gross weight = 8,200 kg.
There was only one Fw 187, the V5, tested with DB601s using evaporative cooling; the only performance figure quoted is 635 km/h (394 mph) "at low altitude", with the engines developing 1,350 hp - there is no indication whether this was with armament or at full loaded weight. It is doubtful whether the RLM would have continued with evaporative cooled DB601s because the system was far too vulnerable to battle damage, not to mention the nightmares of maintenance at a unit level, and supply issues involved in manufacturing and issuing yet another version of the DB601 when there were already problems involved in manufacturing and supplying the standard models. Another problem was that supplies of C3 96 Octane fuel were always problematic and unreliable.
If you have this book and has read it accurate (and the book is accurate translated) I can't understand your claims here, because they are simply wrong!
1. The climb rate you are claiming is with a 1000kg Bomb at external racks, without the 1000kg Bomb it was 18,0m/s; Page 135
2. The FW 187 V5 didn't receive DB 601 H engines, it was flying with the DB 601 V40 + V42 with 1100PS; Page 78
3. The FW 187 V5 didn't flew with an evaporative cooling (Oberflächenverdampfungskühlung), it flew with a Dampfheißkühlung. This system is fundemental different to the He 100 evaporative cooling, where water was circulating through the wings. The system of the FW 187 was an experimental high pressure cooling with very smal convential radiators (no water at the wings)and every later developed engine from DB 605, Jumo 213 and DB 603 received a steam seperator for high pressure cooling. Page 73-78
4. Look at page 81/82 you can see the radiators under the engine.
5. Also there are several reports from pilots about the flight performance of the FW 187 at Rechlin (Page 37) and at Page 95 against a Me 110 with DB 601 engines at Denmark.
I see DonL is going to design a new twin from the Fw 187, with heavier engines, never built, and state that it would not be outclassed by anything, despite that fact that, except for the Mosquito and P-38, there were very few successful day twin fighters. I'd say there might be some interesting development ahead.
I haven't anything designed Mr. GregP the FW 187 was built with DB 601 engines ( FW 187 V5) and the FW 187 was constructed from the scratch to the DB engines, because this was the advertisement of the RLM
The FW 187 V5 flew from 1939 till 1942 and FW was able to receive countless of flight data's and the FW 187 V5 had not a single problem with the g-limit
And the P-38 was faster than the proposed Fw 187 might have been with the proposed DB 601's. The P-38 and some Mosquitoes were at least over 400 mph. The DB engined FW 187 would not have been by a good margin, if you look at power increase alone. Add some frontal area increase and it get slower. You could not substitute a 34% heavier engine with more power without encountering a bigger radiator and the atendant cooling drag increase, not to mention the heavier engine mounts and attendant strengthening of the airframe to support the heavier engines at the g-limit. My estimate with standa aedodynamic equations would have it in the 380 - 385 mph range with the DB 601's. Good, probably. But the best? Maybe.
Mr. Greg P you has realy no clue about what you are writing!
1. The FW 187 was designed to support the heavier engines from the beginning, no modifications are necessary.
2, The change from Jumo 210 engies to DB 601 engines had reduced the drag of the ME 110 significant through much better radiators and resulted in a speed increase of 85km/h with bigger engines.. The FW 187 A0 flew the same radiotors and engines as the Bf 110 B with Jumo 210 engines.
So what do you think would be the speed increase of the FW 187 with the change to the DB 601 engines, if the Bf 110 could increase it's speed about 85 km/h and the FW 187 had the better aerodynamic?
To show you the aerodynamic category of the FW 187 from hard clocked facts/datas, we can compare the FW 187 V1 and the FW 187 V4.
FW 187 V1 single seater
loaded weight: 3.850 kg
Wingspan: 30,00 m²
Wing loading: 128,33 kg/m²
engines: Jumo 210D 2x680 PS
Top speedt 501 kmh at 3.000 m
climb: 17,5 m/s
FW 187 V4 two seater
loaded weight: 4.900 kg
Wingspan: 30,20 m²
Wing loading:165,56 kg/m²
engines: Jumo 210G 2x730 PS
Top speedt 545 kmh at 4.600 m
climb: 12,5 m/s
The main difference were the engines, because the 210G had a two speed supercharger, fuel injection and was the first Jumo 210 with boost effect.
As you can see the FW 187 V4 was 1000kg heavier then the Fw 187 V1, but could increase it's top speed through the better supercharger and boost effect from 500 to 540 km/h.
This is the official specification from FW engineers of the FW 187 with DB 605 engines:
Official specification:
Fw 187 - destroyer/nightfighter from 1942
Wingspan: 15,3
Wing area: 30 qm
Length: 12,45
crew: 2 (200 kg)
empty weight: 5600 kg
take off weight: 8200 kg (with 1 x 1000 kg Bombe)
engine: DB 605
estimated range with internal fuel: 1200 km
estimated range with internal fuel and 900 Liter drop tank: 2100km
Performance:
682 kmh at 7.000m altitude (at 6.620 kg), 658 kmh at 7.000 m with 1000 kg bomb capacity at external racks
547 kmh (at 6.620 kg)at SL
climb rate at SL: 13,0 m/s at 8.200kg (with 1000kg bomg capacity) , 18,0 m/s bei 6.620 kg
climb: 6000m in 5,7 Minuten (with 6.620 kg),
armament:
4 x 151 / 20 with 250 bullets each - fixed to the front
2 x 131 with 450 bullets each - as "Schräge Musik"
1 x MG 81 with 750 bullets - flexible to the back
in summaryt: weapons 392 kg; munition 306 kg)
loading:
maximal 2.000 kg
1 x 1000 kg + 2 x 500 kg or
1 x 1000 kg + 4 x 250 kg or
10 x 50 kg bzw. 10 x AB 23 / 24
With what arguments do you claim that this datas are wrong and a Moussie and a P38 would be faster?
With what arguments do you claim that FW engineers, educated piston engine aircraft engineers are wrong with their official specification, with countless datas of testflights of the FW 187 A0 and FW 187 V5 with DB 601 engines.
From engineers that presented official specifications for the FW 190 A0- A9, FW 190-D9-13, Ta 152 H, FW 200 etc and all this official specification were reached in real-life from production a/c's.
Where is your argument that engineers who worked about 5 years with this a/c can't do a proper official specification but you know it better?
Are you a piston engine aircraft engineer?