RW Mk. III
Airman 1st Class
Ju88 fills that hole if there's no 110.How would the HE 112 compare to the BF 110 in the night fighter role ?
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Ju88 fills that hole if there's no 110.How would the HE 112 compare to the BF 110 in the night fighter role ?
How would the HE 112 compare to the BF 110 in the night fighter role ?
Not the engine, the company. Napier hasn't made anything useful outside of perhaps the Lion. Giving them the business was obviously an attempt at procurement diversification, but the engine was never going to be reliable. Is any museum or racer flying a Sabre today?Not a giant Sabre into a Merlin hole, but Merlins have been swapped into replace Fiat/DB and Allison inlines with little apparent difficulty.
Despite the radiator under the hurricane being designed for a 27L 1500hp engine, not a 36L 2000-2600hp engine.Apparently, it was done, once. According to a chapter of the book, Hurricane (I read this thing about 60 yars ago, so don't press me for details) someone in a Hurri night fighter squadron had his bird loose an engine, and he replaced it with a unit from either a Tiffy or a Tempest; he had great success with it, until the buaurocraps caught up with it, and shut him down. Seems the firewalls on the Hawker fighters were zll the same....
They did the ijaaf a favour there. The Ki100 can be argued to be the best Japanese fighter of the war.Oh, and B-29s over Nihon....
Major problem was lack if suitable strategic targets--Much of Japanese war production was in small shops, even private homes; the factories were mainly assembly centers, not like Western ones, where metal stock goes in a loading dockat one end, and finished aircraft roll out the other. Engine factories seem to have been similar to the Western model--when the one producing engines for the Ki-61 'Tony' was destroyed, they had to replace it with a radial, resulting in the Ki-100(?) 'Tony'
The P-38K's prop required a different gear ratio and different reduction gear casing; the prop centerline was a few inches higher which required a redesign of the engine cowling. That cowling redesign was what would have shut production down for a few weeks. Those few weeks of production loss is why the AAC nixed the P-38K.I think they should have fit the P-38J's with the P-38K's prop -- it seems like it wouldn't be that hard to do. As for the P-61, I think a turbocharger should have been present from the outset -- there were plans to do so, but the twin-stage supercharger was chosen to increase endurance.
What about the Spruce Goose? Heck of a payload.
How hard is it to change the gear-ratio? I remember there was a test run with an F4U-1 with a 0.4 gear-ratio instead of 0.5.The P-38K's prop required a different gear ratio and different reduction gear casing
Why would it matter if the centerline was a little higher or lower, or did it have to do with the shape of the spinner?the prop centerline was a few inches higher which required a redesign of the engine cowling.
And how quickly we managed to get things to work at exactly the right moment... honestly some of it surprises me.From my perspective as an American, looking at American aircraft, I am struck by how many times they made the RIGHT call on aircraft production.
How hard is it to change the gear-ratio? I remember there was a test run with an F4U-1 with a 0.4 gear-ratio instead of 0.5.
Why would it matter if the centerline was a little higher or lower, or did it have to do with the shape of the spinner?
How hard is it to change the gear-ratio? I remember there was a test run with an F4U-1 with a 0.4 gear-ratio instead of 0.5.
Why would it matter if the centerline was a little higher or lower, or did it have to do with the shape of the spinner?
And how quickly we managed to get things to work at exactly the right moment... honestly some of it surprises me.
Despite the sabre weighing a full250kg500kg more before all the oil that goes in it and it's attendant oil cooler.
Despite the radiator under the hurricane being designed for a 27L 1500hp engine, not a 36L 2000-2600hp engine.
Despite the sabre weighing a full 250kg more before all the oil that goes in it and it's attendant oil cooler.
Despite the sabre being 10" wider, with exhausts in a different location. How did they manage the aircraft skin around it?
What about prop? The sabre has a much to0 big prop on it for a Hurricane it would hit the ground on takeoff. So you fit a smaller hurricane prop and somehow the sabre (temperamental engine) performs properly with much less mechanical resistance at the crank.
Also a 2.6 ton 32' aircraft and a 4 ton 42' aircraft have the same firewall??
I have a strong suspicion this story is apocryphal.
There were proposals for a Vulture Engine Hurricane so its not entirely absurd.
The Re 2006 with a DB 603A engine was projected to reach 750 km/h at 7200m (466 mph at 23620 feet)! The first prototype was completed in February 1944 but for political reasons was not flown and was later dismantled.It is very much possible that a Re.2005 prototype have gotten the DB 603A engine some time in 1943, akin to the Re.2006 or G.56; later was good for 425 mph IIRC.
My only thought on 1941/42 is that it was a shame the Soviets didn't get the Cobra 6 months earlier to wring the bugs out of it. Then I'm sure the Americans could have made far better use of it out in the Pacific in 1942/43.From my perspective as an American, looking at American aircraft, I am struck by how many times they made the RIGHT call on aircraft production. After an iffy first year of not being ready for war, the USAAF and USN made good calls that resulted in good aircraft in all categories being produced in large quantities.