drgondog
Major
Just asking, but the tumultuous board meeting in early 1942 where the board denied funds to install "them", was the "them" Merlins or Allisons? Thanks in advance.
Merlins - remember that Allisons were already installed.
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Just asking, but the tumultuous board meeting in early 1942 where the board denied funds to install "them", was the "them" Merlins or Allisons? Thanks in advance.
Right, the P-51 opened with Allisons and I have always wondered why it never got a single stage Merlin before it got the two stage Merlin.
Right, the P-51 opened with Allisons and I have always wondered why it never got a single stage Merlin before it got the two stage Merlin.
You have to look at the timing of the orders for aircraft and the timing of the engine production by Packard.
The Original order for Merlins by Packard was for 9000 engines of which the US was to get 1/3.
Packard did not complete the original order for 9000 single stage engines until the end of Feb 1943. At which time a number of prototypes of the Mustang with 2 stage engines are already flying and 2 stage Merlin powered Mustangs have been ordered in large quantities.
The window of opportunity for a single stage Merlin powered Mustang would have had to have been in early 1942 to late 1942.
However the first 620 Mustangs were British, bought and paid for. The next 150 (Mustang IAs ) were paid for by lend lease and they only rolled out the factory starting in July of 1942 which is about the time the idea of mounting a two stage Merlin begin to get around.
The US is using their share of single stage Merlins in the P-40F at this point. July of 1942 sees Packard hit the 800 engines a month production goal. US is getting around 264 Merlins per month ? US also has no money for fighters which leads to the whole A-36 dive bomber funding trick.
For most of the first 1/2 of 1942 NA is making about 80 Mustangs a month while Curtiss is building over 300 a month (using both Allisons and Merlins)
Between money, production schedules and what planes/engines were ordered when, the window for any sort of single stage Merlin Mustang was very short. And if started in the 2nd half of 1942 might well have delayed the two stage engine project.
I am not in the US at the moment and do not have access to my copy of Rolls Royce and the Merlin, but I believe Rolls Royce was considering installing 20 series Merlins in Mustang airframes. As you note the performance of the 60 series was so superior that the idea was dropped
NAAs board or GMs?You don't have access to the documents that I have.
In late 1940 Kindelberger and Ernie Breech escalated the issues of repeated deficient quality of tech support and failure to deliver by Allison - which was jeopardizing the RAF relationship. Kindelberger contacted R-R in March 1941. Kindelberger sought and received details regarding the Merlin XX/Packard 1650-1. He received a voluminous design package from R-R USA in May 1941. The complaints about delivery and service escalated in late 1941 to a tumultuous Board meeting in early 1942. The Board denied funds to enter into an agreement to install them into a NA-83 series airframe.
When the ARMY got in line with proposed Merlin hybrid experiment during the Rolls Royce conversion in May 1942, they basically stuffed the decision down GM throat. GM tried one last time by forcing NAA to study the issues presented by the Allison 2S/auxiliary 2nd stage but it would have forced a complete re-design and major production disruption.
Take what you wish and leave the rest.
NAAs board or GMs?
I am not in the US at the moment and do not have access to my copy of Rolls Royce and the Merlin, but I believe Rolls Royce was considering installing 20 series Merlins in Mustang airframes. As you note the performance of the 60 series was so superior that the idea was dropped
Can you elaborate on the bench test deficiencies in the -3?NAA was also considering the 1650-1 as noted in my earlier post, and there were still serious positive reasons to go with the 1650-1, namely in Hp to weight and less engineering effort regarding the increased Aftercooling requirements of the 1650-1 vs the Merlin 61 (and 65 which went into the Mustang I conversions). The other issue is that the first 1650-3's experienced bench test deficiencies that in July 1942 - were not easily solvable - pointing to delays to the XP-51B (XP-78 at that time) first flight and subsequent production run. Those issues remained in October 1942, which did in fact delay the XP-51B and also delivery of the 1650-3 from 'scheduled' from February to 'actual' May 1943.
Shaking out initial production release of the 1650-3 combined with the Packard strike in June/July 1943 was the real root cause for the P-51B not beginning ops about the time the 55th FG started combat ops with P-38H in mid October 1943.
The primary issues for the first series of Bench tests at Wright Field were piston/crankshaft failures at 12 pounds/54" boost as well as inadequate carburetion for projected 61".Can you elaborate on the bench test deficiencies in the -3?
A strike in wartime? How did that happen?