drgondog
Major
IMO - Steve is correct. Pre-1939 all or nearly all fighter aviation was Pursuit/Interceptor -------------> fast, climb fast, turn tight to best the opposing challengers for battlefield superiority or air defense of the homeland.
Those design objectives dictated HP available to HP required and wing loading discussions - fuel was placed in the fuselage to optimize roll and armament options.
Long range escort was deemed impossible for single engine fighters because the necessary fuel fractions were too high to maintain climb and maneuverability goals with existing engines. High altitude performance objectives dictated turbo superchargers for AAF for Interceptor role, and basically ignored by USN as not necessary for fleet operations scenarios of the day. Two stage/two speed superchargers were conceptualized but not in practical stages of development.
The Mustang broke ground on fuel storage in the wings - not because of foresight but because the Meredith Effect advantages to drag reduction was a REQUIRED part of both the original P-509 proposal to AFPC but maintained center stage during the development of the NA-73 Specifications. No room for fuel in the fuselage (or so they thought) because the stability and control issues were deemed a major issue to successful development and acceptance from RAF.
That said, the RAF continued to press NAA for more range options leading NAA to develop auxiliary fuel cells to occupy the gun bay/ammo chute section of the wing. It was tested and put into production as kits for an extra $25/per aircraft. With the fuel cells and two remaining cowl mounted 50 caliber guns, the Mustang I was capable of 1500 miles straight line range, about a 50% increase over existing capability. Projected Combat Radius was London to Berlin (in 1940). Not very practical for intruder type missions but an excellent option for Recon. I have not found docs to support operational use as extended range recon but the installation and maintenance instructions were all in RAF Mustang I Maintenance Manuals.
IMO the RAF get perhaps a little too much credit for the design attributes of NA-73, but perhaps a little less credit than they deserve for the impetus of NAA to craft many improvements to the operability and handling qualities of the P-51 with constant flow of suggestions and issue documentation coming from RAE and combat ops experience.
Those design objectives dictated HP available to HP required and wing loading discussions - fuel was placed in the fuselage to optimize roll and armament options.
Long range escort was deemed impossible for single engine fighters because the necessary fuel fractions were too high to maintain climb and maneuverability goals with existing engines. High altitude performance objectives dictated turbo superchargers for AAF for Interceptor role, and basically ignored by USN as not necessary for fleet operations scenarios of the day. Two stage/two speed superchargers were conceptualized but not in practical stages of development.
The Mustang broke ground on fuel storage in the wings - not because of foresight but because the Meredith Effect advantages to drag reduction was a REQUIRED part of both the original P-509 proposal to AFPC but maintained center stage during the development of the NA-73 Specifications. No room for fuel in the fuselage (or so they thought) because the stability and control issues were deemed a major issue to successful development and acceptance from RAF.
That said, the RAF continued to press NAA for more range options leading NAA to develop auxiliary fuel cells to occupy the gun bay/ammo chute section of the wing. It was tested and put into production as kits for an extra $25/per aircraft. With the fuel cells and two remaining cowl mounted 50 caliber guns, the Mustang I was capable of 1500 miles straight line range, about a 50% increase over existing capability. Projected Combat Radius was London to Berlin (in 1940). Not very practical for intruder type missions but an excellent option for Recon. I have not found docs to support operational use as extended range recon but the installation and maintenance instructions were all in RAF Mustang I Maintenance Manuals.
IMO the RAF get perhaps a little too much credit for the design attributes of NA-73, but perhaps a little less credit than they deserve for the impetus of NAA to craft many improvements to the operability and handling qualities of the P-51 with constant flow of suggestions and issue documentation coming from RAE and combat ops experience.