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The ground fiction model is pretty off in general. You should for example be able to taxi in idle for low weights but right now even a clean jet will require about 75- 80%N2 to keep taxiing in DCS. 

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Yup, the current model is sort of a workaround, and a compromise between being glued to the tarmac and sliding all over the place.
The Mirage 2000 should be able to taxi in idle, so does the F-16, and today I heard an interview with a former F-15 pilot saying that one could even reach 80 knots in idle.

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Except wheel to surface friction is diffrent from brake load friction from what I can tell. So it's about thrust vs the brakes not thrust vs rolling friction. In that case, the brakes are weaker to make up for the overdone rolling friction. Meaning with too much thrust the sim "lets" the wheels roll when it shouldn't. 

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When NATOPS refers to "nozzle position 2" it may actually be referring to Zone 1 AB. "Minimum zone afterburning" would be Zone 1, as Zone 2 would be one step above minimum. It also specifically says "nozzle position," and nozzle positions are not equivalent to the AB zones. 

 

AB Zone NOZ POS
1 1.5
2 2.4
3 3.2
4 4.0
5 4.3 ~ 5.0

 

If 2.4 is the minimum NOZ POS for Zone 2 AB, then NOZ POS 2 would still be Zone 1, I assume. I haven't checked the nozzle gauge specifically, but in an unladen Tomcat the brakes have mostly held through Zone 1 in my experience, so it shouldn't be that far off even with our FUBAR'd ground physics in DCS.


Edited by Nealius
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Quote

The ground fiction model is pretty off in general. You should for example be able to taxi in idle for low weights but right now even a clean jet will require about 75- 80%N2 to keep taxiing in DCS. 

 

This is fairly worrying, it seems very common now that we're finding things that seem to be implemented using bailing wire and duct tape owing to the engine just not supporting these things. 

 

I think ED does a pretty decent job with the duct tape and the bailing wire, but the limitations of DCS seem ever present. 


Edited by Northstar98
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This has been known for years back at this point. Worst part is the guy who wrote all the original code died, so it's basically a forensics project just to find out HOW something works, and also why changing totally unrelated things breaks other parts. Because they give the Toy Core away free, and the Pro training product doesn't really need a lot of that stuff to work to do its job as a task trainer, there just isn't the business case to Start off with a new modern layered middleware style rewrite. 

 

They say they're going to do that for M.A.C., but my guess is it will just be another Jenga tower stack iteration of Lock On. If that is, it ever happens.

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Nealius while what you said about nozzle position vs zone is correct, the brakes are still under performing significantly. Here are the current tested limits.

 

F-14A brake limit tested at max gross weight, dry paved level surface, 12/16/2020:

 

Single engine (anti skid on): Zone 1

 

Single engine (anti skid off): MIL

 

Dual Engine (anti skid off/on): 90%

 

 

This issue coupled with the exaggerated asymmetric AB lightoff/staging make shore afterburner takeoffs more unstable than they should be.

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