Cowboy1968
Charter Member


Doing the conversion work on the P-59 had got me to thinking about the machine really on a whole. Was it a bad plane or a good plane: Should it have seen action?
Well as we all know its top performance was equal to the P-51D Mustang. It had similar top speed. It was as maneuverable, maybe even to a point of being disadvantaged, because of the machines tendency to over react to pilot input. It had a good armament and a decent range for a first generation jet. Though in the face of the perfomance figures the Army Air Force was disappointed in the machine. They were hoping for a machine that could out perform any US piston engine type avalible. They didn't get that on paper.
In practicality they did....
I say that because after doing some flying in both machines in our sim and reading, yes reading operational manuals i have in my collection, I have some thoughts.
1. Even though both planes could reach over 400 mph at full throttle, the limitations of the P-51 were clear. According to the manuals i have on the P-51, it could only be flown at full throttle at max rpm for no more then 5 minutes before things could go wrong. The P-51D had a military rating of 3,000 rpm at 61 inches of manifold pressure. This put a strain on the Packard engine, and this was the way to achieve top speed. The Packard engine was designed to have a Max Continuous rating of 46 inches of MP and only 2,700 rpm. At around 5,000 ft. the Mustang achieves an IAS of aprox. 247 knots in Max Continuous rating. When you take the P-51 up to its Military Power then your speed becomes 299 knots. And as i said this could only be maintained at these setting for five to ten minutes.
Now the P-59 shows the big step jet engines were from piston engines. At full throttle at 5,000 feet the Airacomet could maintain an IAS of 324 knots. The P-59 could maintain this power setting for fifteen minutes on the engines. Its Max Continuous Rating was set at 95% of the engine's turbine rpm. This gives her a IAS of 304 knots. though to conserve fuel the airplane had a economic cruise of 196 knots at 60% RPM. While the Mustang cruised at 42 " Manifold Pressure on 2,400 rpm for a IAS of 217 knots. The Mustang had a service ceiling 41,900 ft compared to the Airacomet at 46,200 ft. The P-59 could out climb and out run the Mustang on most accounts, but its lack of range and the fact that it wasn't the significant improvement the Army wanted it wasn't put into combat. The P-59 even with drop tanks lacked the range, like most early jets, it has to be considered a point defense machine with a limited offensive capacity due to its short legs.
Though the P-59 did show the advantage of jet over piston engine in flight. At altitude the P-59 didn't loose any of its thrust, while the P-51 lost horsepower the higher it got toward its service ceiling, but that advantage didn't out weigh the limitations on the General Electric torbojet engines. Those disadvantages didn't only include high fuel consumption, but it also had more maintenance headaches. The engines required overhaul far more quickly then the Packard V-1650 of the Mustang.
In my humble opinion though, the P-59 should have been deployed for service at least in the Pacific or the MTO....
That is just my thoughts on both of these wonderful machines.