wmaxt
Staff Sergeant
Glider said:Do we know if these changes or at least some of them were made on later versions of the plane?
Yes, many changes were made to the systems of the later P-38s
1. Two generators were added with the early J's - the single generator is singled out by Art Heiden as one of the worst problems for the early P-38s because the props were electrically controlled.
2, Turbo controls became automatic in the Js.
3. Cooling flaps became automatic with manual override in the J models - major engine and turbo problems esp at altitude were directly related to cold (~130deg oil at the engine) engine oil, mostly resulting from improper operating techniques.
4, Prop/mixture controls were simplified. a two setting mixture control was implemented in the H and Lockheed had a unified prop/mixture/throttle control designed but was denied permission to install it by the War Production Board.
5, Fuel system was redone to provide crossfeed from any internal tank to either engine.
6, heat ducting to the cockpit was redesigned for the J-25 and L models.
7, Hydraulic controls for the ailerons.
8, Almost forgot one of the most important, Intercoolers were changed to core type with auto temp control on the Js eliminating the too cool/overheated air issues the earlier aircraft had, and eliminating both a cockpit load and increasing hp by ~250hp each engine (the H had the same engines as the J but the intercoolers allowed full output).
As Colonel Rau mentioned the performance of the P-38 was great but the experience with combat and twin engines to low time pilots with inadequate training was a very great issue. As Flyboy pointed out the controls weren't that different from any other fighter of that era.
wmaxt