" The first F-16A ADF conversion was completed in February 1989, while a contract was placed for kits to update and modify a total of 270 F-16A/B’s at the Ogden Air Logistics Center in Utah. The Block 15 airframes used for the ADF program were all meant to be upgraded to block 15OCU standard, and both programs ran in conjunction. Aircraft entering the Ogden ALC for ADF upgrade also received the Block 15OCU avionics installation. The net result is that all ADF aircraft are Block 15OCU airframes. The last ADF left Ogden in 1992."
The propulsion section consists of a launch motor and a dual-thrust
flight motor. The launch motor ejects the missile from the launch
tube. The missile coasts a safe distance (about 9 meters) from the
gunner before the dual thrust flight motor ignites and provides a
sustained 22 gravity acceleration that arms the missile.
Such a great source showing us how Stinger can accelerate at 22Gs, now find me something that states the actual average G load of the missile. But now at least read what the source is talking about before telling me I shouldn’t listen to RU propaganda.
Who should I listen to ? Random guy on a forum that can’t comprehend three simple sentences in English ? No thanks.
Sure, but that doent justify using a out of context quote to prove a point, and at least gaijin still use the same metric for all manpads which has this kind of guidance, which also affect the more modern russian missiles.