F-15 Eagle: History, Performance & Discussion

Designation Systems claims that the ALQ-127 was used on the B-52G and E-3 airframes and was replaced by the ALQ-153; which is known to be a Pulse-Doppler MAWS system.

Though the -153 was integrated into some ECM pods(ALQ-131 & -184), which might be the F-15 specific(All variant) carriage method, though would depend on the pod being correctly configured.

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I have a manual for TEWS, year 2000, it has a lot of pages but I will go through it when I have time.

Maybe i saw it, but the secret has been erased from it

This doesn’t seem to be accurate. No F-15’s SEP = 0 curve looks like that with an air superiority load unless it’s flying in arctic conditions.

Nothing there.

AN/APG-63(v)2が2000年10月より前にIOCに達したという資料はありますか?私が調べた限り2000年12月だと思いますが。

I don’t know what you’re responding to

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hey now i cringe for some of you debating “whose got the first AESA radar” on both side here, now you just name calling. that’s not cool, as i see it the argument is redundant as it is and stearing to the offtopics stuff with F-2 so chill out and stop it.

@warabimotis @warthogboy09

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For me, gaijin not ready F-15C MSIP II with AN/APG-62(V)2 or AN/APG-63(V)3 AESA radar in 2 or 3 years

I predict from first devblog season it might F-15C MSIP II with AN/APG-63(V)1 radar, AIM-9 sidewinder (AIM-9M & AIM-9M-9) and MRAAM (SARH) AIM-7M Sparrow & (ARH) AIM-120 AMRAAM (AIM-120B & AIM-120C-3)

1.) it is on topic. It refers to the F-15.

2.) boohoo

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The graph you posted?

G or instantaneous turn rate ?

IMG_3326
This

This is not a graph of sustainable G but of “allowed” ( or instant G) for the OWS system.The F-15 has a soft limit on overload, so it can go above the G in the figure.
Without the OWS system, the limit is 7.33, but - again, it is not a hard overload limit. Nothing will limit the pilot if he pulls too much.

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Ahhh then those are speed limits my bad.

The figure shows the flight envelope of the allowable overload.

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your wish has been granted :)

Sustainable G is pictured here for the F-15A, 97% of the trim says it is reduced thrust.

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Can I see the cover of that document to be sure rules aren’t being broken.

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