One of the issues with the chapters discussed so far is how static they are. Although they provide a good picture of the “new” AIM-54 Phoenix, this study would be relatively incomplete without testing more complex situations.
Here is the first scenario: “zero-cut” or 180 HCA / DTG.
The updated AIM-54 “resets” the differences between different rocket motors. Since they were a means to differentiate the supply, and the Mk60 ceased production in the late 70s, this decision makes a lot of sense, in my opinion.
Part II highlighted how the altitude reached by the new missile is lower, and manual loft compensates for this drawback. Ergo, the new missile takes full advantage of the reduced drag and improved rocket motor when employed in such a manner.
After the brief overview of the previous chapter, it is time to check how the missile performs in detail, starting from the simplest scenario: 0TA/ATA, at different ranges, and altitudes. Unfortunately, as we will soon find out, the Phoenix is all except “simple”.
This is a brief look at the updated AIM-54 Phoenix, released in March 2026. Later on, if there is enough interest, I will prepare the usual load of charts and data in more detail.
An impromptu series of considerations after a casual training session. Probably nothing new to F-4 and F-14 players, but perhaps some points will trigger an interesting discussion with your crew.
