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If the Sabre works, who needs the Centaurus and Bristol are free to concentrate on manufacture of the Hercules and development of the Orion?The funny thing is some of Fedden's engineers had to be seconded to Napier to fix problems with the Sabre's sleeves. The question become's was the Centaurus sufficiently sorted to become a contender due to production problems and availability of the Sabre as well? (Fedden was at Bristol long enough to start the Orion as well. And I believe the Centaurus was in production by '43.) The Centaurus may have been a Hobson's choice.
I'm curious as to what range and endurance specs were required for the design. I ask because I only have Tony Buttler's book to go on and it reveals litte.
That's very informative, and so forth. That said, what range and specifications were stipulated for the design.The Firebrand had a 168IG main tank, and a 71IG aux internal tank, and a range on max internal fuel of 745m @ 256mph at 10kft. There were provisions for twin external drop tanks of 45IG capacity, each, and/or a 100IG centreline DT in lieu of a torpedo. (Wings of the Navy)
That's very informative, and so forth. That said, what range and specifications were stipulated for the design.
Say, I issue a specification for 750 miles at 250 mph. The plane might have a range of 900 miles at 300 mph, but that's not the original specs.
It's all about availability, money and needs. The Centaurus was a bird in hand. Remember it ran in the late '30's. In fact, I think it beat the Griffon by a fair amount of time.If the Sabre works, who needs the Centaurus and Bristol are free to concentrate on manufacture of the Hercules and development of the Orion?
nuuumannn ,
Now this is the kind of information I was looking for
This is an interesting set of requirements: I'm not sure how many aircraft were stipulated to have this level of endurance that I know of (other than the P-61); as for the requirement for 10 minutes of maximum power: What settings are we talking about? MCP is largely indefinite for individual flight purposes; Military Power is usually based on 30 minutes of operation; Emergency Power is usually based on 5 minutes.
- Endurance of 4 hours at 120 knots or greater @ 15000' or greater altitude on internal fuel
- Provision for 2 additional hours endurance at the same speeds and altitudes as before, preferably in a separate (and internal tank)
- 10 minutes at maximum power @ S/L
My guess is that they wanted an overload tank rather than drop tanks so they don't have to carry all of them onboard.
I'm curious what typical endurance requirements were required for other aircraft such as
From what I remember, the P-51B/D seemed to see around 6 hours in the air...
- The Fairey Firefly
- The Curtiss P-40
- The Grumman F6F Hellcat
- The Chance-Vought F4U Corsair
Calling the experts...
drgondog fubar57 S Shortround6 swampyankee W wuzak X XBe02Drvr
Easy to land though.Actually that is why you pay test pilots. To have an opinion. Many test pilots had degrees in engineering or lots of practical experience so they could give feedback to the engineers in technical terms and not truly helpful (not) comments like "it stinks and flys like a barge".
And that usually involved flying at speeds of around 300 mph if I recall...drgondog said:The P-51B/D combat mission endurance was at least 8 hours
Was Blackburn known producing aircraft that were excessively heavy, or clunky?