/\This. Some other issues too. Great writeup here...Trouble with the Spit is they picked up speed too fast in the dive.
SPITBOMBER — Vintage Wings of Canada
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/\This. Some other issues too. Great writeup here...Trouble with the Spit is they picked up speed too fast in the dive.
Britain had no problems in installing the good propellers on their bombers, so they should be okay. There is a lot of dead or obsolescent wood around that deserves the axe, so our brave new fast bomber materializes.for the 1939 Suizei class of bombers is that only 2 countries had a 1000hp/15,000ft engine. a few others had works in progress. and there were few hiccups.
Britain, got the 1000hp engine, doesn't have enough propellers or at least good ones.
France, no 1000hp engine, working on it.
Italy, no 1000hp engine.
Japan, no 1000 hp engine (license signed in 1938, Prototype D4Ys used imported DB 600s in 1941, production planes in 1942, a little late)
Soviet Union. M-103s or a handful of M-104s? According to one source 50 M-105s built by the end of 1940.
US, 1000hp engine in 1939? got the design, got 40 engines by New Years Day 1940. rebuilding several hundred engines in the summer/fall of 1940 to meet spec.
With 1000hp engines there is only so much trading off you can do. With 1300-1400hp engines you can do a lot more because a lot of you other "payload" is the same.
Two man crew (?) 200kg, cockpit structure, instruments, 50-70kg of radio gear, rear gun? crew armor.
All the same for the 1000hp plane and the 1400hp plane (or mostly) so you have more power to get the bombs and fuel off the ground even if you use a bit bigger wing.
US has the best chance at a semi fast radial engine bomber
The R-1830 offers about 1000hp at 14,500ft with a two speed supercharger and some abuse to the engine. At least the engine is under 50 in (1.27m). A 55in radial engine has about 20% more frontal area.
Also the rate of progress for somethings was rather quick in some ways and not so quick in others. It took about about 8 years for the US to go from installing flaps on the P-26 to the Douglas A-26 flying with double slotted flaps (another 2 years to go into service). Sometimes if you start too early you are stuck with old airfoils, structures and systems.
Again, what do you want the plane to do?
dive bombing caught peoples imagination, how practical it was for 'close support' is subject to question. Trying to spot targets in woods/forest from 10-12,000ft is not easy. It isn't easy trying to do it from under 500ft either.
Bombing stuff in the desert or in large grass lands is a lot easier.
M-62(1040 hp), M-63 (1100hp), M-88(R, 1100hp) - mass production in 1939, M-87(950hp) - in 1938.Soviet Union. M-103s or a handful of M-104s? According to one source 50 M-105s built by the end of 1940.
Note that stipulated altitude is 15000 ft, ie. about 4500m. Here the M-62 and -63 don't break the 900 HP mark, so a nod against these.M-62(1040 hp), M-63 (1100hp), M-88(R, 1100hp) - mass production in 1939, M-87(950hp) - in 1938.
Ok, but is it principal? SZ-2 M-62 (pre-Su-2) reached 403 kph at 4700m. It could take up to 500 kg bomb loading (2xFAB-250), but it was not tested in this configuration - a new engine type was installed.Note that stipulated altitude is 15000 ft, ie. about 4500m. Here the M-62 and -63 don't break the 900 HP mark, so a nod against these.
The I-207 equipped with M-63 could be used as a dive bomber like SBD. Or even more efficient taking into account its size and weight characteristics. SBD was not optimal for the Soviets. They needed either a good level bomber (Tu-2) or a fighter-bomber for dive bombing. The story of the Su-2 clearly demonstrates it.A 9 cyl engine will have more drag than the 14 cyl engine of the same power and day, and much more drag than a V12. A V12 will also get more help with the exhaust thrust in the installations from 1939.
The two/three minuses combined mean that M-62 and M-63 should've been avoided on a fast-ish bomber, that SR6 and I were discussing a few pages on now.
468 kph at 5200m - not bad for April, 1939.The M-87 would've been a tad better than the 9 cylinders, without the bulk and with a bit more power (950 HP at 4.5 km).
Good source for M-88(B?) being in mass production in 1939?
Okay, thank you.
"Russian Piston Aero Engines" by V.Kotelnikov