Part 5.03 The Butterflies falter slightly.
As to progress at Power Jets, Sir Phillip had already done battle with the Treasury over adequate funding and the purse strings had been eased at least to match the funding given to Metropolitan-Vickers. Power Jets had made steady progress and after the burn out of their first concept engine Whittle had moved on to build a full scale engine test engine with multiple burner cans. This was due to start testing soon but Whittle was realistic in how long it would take to develop the design to the point where a flight worthy example could be produce. He stated however that what he was aiming to achieve with this ground test engine was sufficient thrust for a powered aircraft and sufficient reliability to prove the viability of a flight worthy engine.
Engines were, it seemed taking up an inordinate amount of Sir Phillip’s and the AM time. His latest meeting with Earnest Hives from RR had been encouraging regarding the Merlin but the lack of progress with the Peregrine and the Vulture was a worry as there were a number of projects relying on those engines. Currently RR were working on the, Peregrine, Vulture, Exe and Griffin, as well as continued development of the Merlin. Combine this with the efforts to get the new plant at Crewe on line and plan for the Glasgow factory Sir Phillip was convinced that RR was especially, on the engineering front overextended. In his opinion some hard discussions over what to cut would have to take place and decisions made soon.
The News from Bristol’s was no better the Taurus was showing an alarming propensity to turn itself into molten scrap and the Hercules was faring little better. The problems with both the Peregrine had implications for the Whirlwind, whilst the Taurus would effect, The Beufort, The Gloster F5/34 now christened the Guardian, The Gloster F9/37 and the Navy’s Albacore. Further they had planned to re-engine the Bristol 148 with a Taurus engine for comparative trials which were apparently of great interest to Sir Arthur Dowding and Naval Aviation team.
With Armstrong Siddley Motors (ASM) still having serious problems with all their dog series of inline radial engines (dog by name dog by nature) ASM’s Dearhound motor had been in design and development since 1935 and as of early 1938 had failed to pass a single test. Lt. Col. F. L. R. Fell, the head designer admitted that the engine would need a complete redesign if it was to ever produce its forecasted output of 1,500 hp (1,119 kW) the engine displaced 2,330 cu in (38.18 L). The Col wanted to produce a liquid cooled engine but the board of ASM insisted on air cooling only. Alvis had the Pelides in limited production as they prepared to ramp up production and further the first hand built Alcides were doing well on the test stand and a pair were due to be test flown before Easter.
The development of this large capacity engine 54.24 litres had been remarkably quick. This had been much facilitated by the simple fact that it’s 18 cylinders not only shared the same 146mm bore as the 14 cylnder Pelides but also the entire cylinder head, valves, OH. camshaft, camshaft drive and cylinder. The difference in stroke between the two engines was 180mm for the Alcides and 165mm for the Pelides, this difference being accommodated by the longer steel cylinder liners used on the Alcides. On the test stand the un-super charged Alcides was getting close to it’s calculated rated horse power of 1300 and had attained a maximum of 1500Hp. These power figures were based on rated altitude of 5,000 and would need to be verified by flight testing. The supercharged version known as the Alcides Major should be able to achieve a rated power of 1225 Hp at 13,000 ft with a maximum pawer of 1,375Hp. Weighing 1,645 pounds and with a diameter of 55.5 inches the Alcides was a big engine but comparable with the Bristol Hercules on all important parameters. So as to not interrupt Alvis in getting the Pelides into series production in their factory the Alcides production would be undertaken by Armstong Siddley. All AM funding for the dog series of engines would be transferred to the Alcides development.
RR’s problems with the Vulture would effect both the Hawker Tornado, Martin Baker MB3 and the Manchester. With the Sabre engine doing well on the test stand Sir Phillip could only hope that it could be got into production sooner rather than later. As an alternative he would request that both Avro and Hawker take a look at substituting the Fairey Monarch for the RR Vulture. Now the trick was to find substitute for the other engine type causing problems. The Beufort could take the Alvis Pelides (the Bristol Cousins not withstanding) and the Albacore could as well if needed. The Gloster Guardian and the Bristol 148 like wise could take the Alvis engine. Being just a bit lighter than the Follond NF1 the Guardian had the margin on performance. The test pilots at Martlesham were comparing the difference between the two aircraft performance as on par with that between the Spitfire and the Hurricane. The Gloster F9/37 could also be adapted to take the Alvis Pelides. The problem would be ensuring sufficient production at both Alvis and Fairey’s to supply this increased demand if and when these aircraft entered service. So early in 1938 the staff at the AM were burning the midnight oil seeking solutions to the engine production back log.