No civilian aircraft is ever at its maximum popularity just a couple of years after entering service, which is when the Comet crashes happened. Also, since it was the Comet I that crashed, and they came out with the Comet IV more than 4 years later, I suspect it wasn't quite as limited as it might have been otherwise, though I agree the design had its limits.The Comet was as successful as it was going to be.
However, like the comet, those accidents lost it the confidence of the public.An American turbo-prop airliner was stricken with catastrophic aircraft failure and went on to lead a phenominally long life as the P3 Orion.
However, like the comet, those accidents lost it the confidence of the public.
Which is where I have a problem - they went for the lightest structure they thought they could get away with, in a situation where they had next to no empirical data. That sets off all sorts of alarm bells in me as an engineer - particularly as they did their proof testing to confirm that it worked OK in service with live passengers!Lots of hindsight allowed people to point to things afterwards and join dots that were barely visible on the paper at the time of design. What De Havilland were doing for the first ever time was high altitude civilian flights with pressurisation and depressurisation cycles several times a day for days on end. This doesn't happen to military flights. They fly far less often and with a simple out and return profile. There was no comparison for De Havilland to turn to.
Hardly a surprise - it's a 10 years older aircraft design!But let's say de Havilland knew of the dangers of metal fatigue of repeated flying to and from over 30,000 feet cruising altitude and designed the skin structure and windows properly. It would have enjoyed more success, but the limitations of the Comet design--especially with the engines buried in the wing roots, instead of the podded installation pioneered by the B-47--would have limited the growth potential of the basic design to effectively what became the Comet 4 of 1957. And the Comet 4's passenger/cargo capacity, speed and range would still be inferior to the Boeing 707-320 Intercontinental that arrived in 1960.
Not sure - the VC-10 had a lot in common with the VC-7 (V-1000). It may well still have existed as a development of the VC-7, or the next model along.(By the way, one wonders what would have happened had the Vicker V1000 actually been fully developed and powered by Rolls-Royce Conway turbofans? Would it have mean not only a true 707-320B competitor, but we would have never seen the VC10 with its tail-mounted engines?)
That I really, really doubt - it's very simple structural engineering indeed. Remember that wing structure is only one of the things being considered - engine out performance for instance is another major one, and there putting the engines as close as possible to the centreline is a bit requirement. In the very early days of jet aviation when they were far less reliable than today and the available thrust was marginal, that had to be a major factor.Podded engines also provide a structural advantage by spacing the weight of the engines over a greater span and reducing bending moments on the wing spar roots.
Propeller-driven transports an bombers did that to provide clearance between all the propellers. Apparently early (multi-engine) jet designers did not understand the concept and had to re-learn how distribute the load of engines and fuel.
Well they already had the Comet 1A in service, were working on the slightly enlarged longer ranger Comet 2 in 1953 and had the enlarged Comet 3 test flying in mid-1954 so obviously quickly realised the need to grow it. If we say it takes a year to get it into production and service that gives de Havilland a window of two and a half years before the Boeing 707 has its first test flight. Pan Am and Eastern Airlines were apparently interested in the Comet, if de Havilland can deliver them an enlarged version soon enough to be seen to crack the US market and before waiting for Boeing is a viable option do people think an extra fifty to a hundred planes sold would be completely unbelievable?So what constitutes success for the Comet, if double the number were built? Triple? If they had stayed in revenue service longer?
Just to be pedantic; the B36 reference was to the long runways it needed not to the wings or indeed the aeroplane itself at all.The Convair B-36 Peacemaker was made by Ta Da Convair not Boeing. It is the worst possible example of a thin wing you could come up with.
Just to be pedantic; the B36 reference was to the long runways it needed not to the wings or indeed the aeroplane itself at all.
More likely BAE as I can't see de Havilland managing to stay independent up to modern times, the financial and government pressures to merge would just be too great. I think they could maybe have sold 200-250, maybe 300 at the most, before they reached the maximum they could do with the design and had to start afresh. The various British aviation companies did have a wide range of models and ideas that could have covered the market if things had been handled somewhat better.If de Havilland were truly successful, Airbus might never get off the ground. In the perfect alternate timeline, de Havilland would currently build four or five different sizes of jet airliners to serve different routes.
It wouldn't be non-stop, the Comet 4 just like the early Boeing 707s and Douglas DC-8s needed to go via Gander in Canada when travelling westwards due to the prevailing headwinds IIRC. The 707 didn't have the range to make the journey in one go until the stretched 707-320 variant came into service in mid-1959.