So 5 min low thrust for prep and taxing, 10 min full ab and regular USAF prescribed reserve being 20 min loiter AND 5% of max fuel. So roughly 100 + a few tons + 400 kg + 400 kg
Here’s thunderbirds manual. http://afthunderbirds.com/site/wp-content/uploads/2012/04/2015-Support-Manual.pdf
They say one f16 needs approx. 800 gallons per show flight. That’s some 2,4 tons. F-35, being roughly 60% heavier would, also very roughly, consume 3,8 tons of fuel.
Whatever the F-16 needs, it carries 6,000lbs of fuel for a staged airshow, 5,000lbs for a high show, and 4,000lbs for a low show. (staged i.e. not taking off from the site of the airshow). Considering the only USAF F-35 air shows are part of the heritage flights which require 18,000lbs of fuel, the standard fuel load for future F-35 air shows may not be established yet. The Dutch may have different fuel requirements for air shows, so who knows how much fuel the F-35’s were carrying in the above video.
standard, i.e. there are no airspace, weather constrictions that would cause them to compress time or delete maneuvers.
You really should stop, each maneuver is spelled out in the manual, as well as “in case of” Abnormal procedures . No, I don’t have a favorite jet, I’m not you with a flanker crush. I quoted you exactly what the manual said. All I see is you trying to weasel out of your assumption because you have some odd bias that makes it impossible for you to accept anything about U.S. fighter aircraft that does not fit your preconceived notions (even when it’s from official documents).
Disengenuous, and sour grapes. You got called out for making assumptions, leave it . The only time it flies with less than full fuel is a short display. Standard display- which you can read- flown with an impressive 18,000 lbs.
Don’t care what Sukhoi’s fly with, just care that your point was B.S.
Funny how the LM F-35 get the Airshow rubbish stamp.
But back track into the mid 2000 when LM F-22 made its first flight display, there was so much entusiasm..
And even now we start getting the same BS speculation that both F-22 and F-35 are doing flight display with full internal fuel and weapon suite like its the “norm” of things..
Well, that because you have no clue what you are talking about. Look up the USAF airshow regulations. Then possibly you will start to understand that the only “BS speculation” comes from A) people citing airshows as a example, or non-example of capability B) people making comments when they have no clue about what the regulations are (see yours above)
Edit- here I’ll do it for you:
These maneuvers will be flown in a standard configured aircraft with a full fuel load of 18,000 pounds at engine start. If mission needs dictate, taking off with less than full fuel is authorized. Under all circumstances, the pilot must takeoff with enough fuel to execute the profile and divert if necessary. Inert weapons may be loaded, however if the total weight exceeds 1,000 pounds the total fuel at takeoff must be less than 17,000 pounds.
http://static.e-publishing.af.mil/production/1/af_a3_5/publication/afi11-246v1/afi11-246v1.pdf
Super, can’t wait for months of airshow armchair “analysis”, and the ensuing pointless arguments.
Air S-H-O-W
A random thought just popped into my head. I wonder if the new carriers could take a C-130? I’m sure it’s possible, the cousins did it years ago.
.
https://www.youtube.com/watch?v=ar-poc38C84
Guy had some stones, going to have to look up backstory on how many knots the Forrestal was generating to make that landing possible.
Edit- 40 to 50 knot WOD- ship speed not mentioned.
Ehm, gun in A version is internal, so I guess it should not be counted.
Said so, just crossmatching such numbers leave me quite suspicious about the 9G pretense at the (not operatively realistic) 100% fuel: not about the fact it can make it trought phisically: just about how it would end up in terms of speed and energy after having performed it…
There is literally almost nothing accurate in the figures parlay posted. Seriously, the empty weight is easy to find accurately, yet his is off by over 1000lbs. Just numbers pulled out of a hat
The Defense Minister who cries the Rafale:
“Our LCA Tejas is just as cable as the overpriced Rafale with the only 1/5 to 1/6 unit cost of later.”
“We will soooooo~~~n select a good foreign fighter to be made domestically by the end of this fiscal year. The possible candidates include the overpriced Rafale, the over-overpriced Eurofighter, the dwarfed Gripen that is no better than our little beautiful Tejas, and the underpowered and outdated Superbug……”
Which begs the obvious question, “why select a foreign fighter at all if Tejas is so capable”? No offense, but thank goodness fo India’s government-MoD bungling. Makes people living in the US look a bit more fondly upon our own disfunctuonal DoD, Congress.
Granted, it is said that F-35 comes with a higher wing loading, so it could be true.
But again what is the NTOW and MTOW of F-35A?
What do you want? Loaded weight or operating empty weight (OEW)? MTOW is 70,000lb class.
Integrate? Look, it doesn’t work like so.
The sole thing you have to integrate is something called balistical computer, in case of Russians is usually a SVP-24, that will calcolate in real time the point of impact of your weapon i.e. the more the less similar computers do on MBT and artillery system, just a little more complicated given the higher speed involved.
“Integration” of a new bomb or rocket is made in the same way used with said system: going to an aerial poligon and dropping them until a sufficient exhaustive database is collected.
Hate jumping in this mess, but no, integration is just not that easy. There are captive carry vibration tests, computer modeling, separation tests ( single weapon, stores interaction). While much of can be done using virtual modeling, shaker test stands, and such, live testing is required and it’s not free. It still adds test flights to a development program.
Something is very off here.. What is the NTOW of F-35A?
I suspect the Full fuel quote is at 55-65% fuel fraction range at 9G.
Nope, you’d be wrong. Several posters with selective reading. How do you outright dismiss the statements from Lockheed VP O’bryan clearly stating 9g with full fuel and missiles in the AFA’s own magazine? Then read the DOT&E and completely ignore parts from all three variants:
F-35C-full block 2b(partial envelope compared to 3F) 6g available with 93% fuel. Flight testing to full 7.5g block 3F with fuel monitoring system being conducted.
F-35B-full block 2b(partial envelope compared to 3f) 5.5g available with 96% fuel. Flight testing to clear full block 3F.
F-35A- posted above.
Now, if you cannot understand that the full g envelope for all three variants is at full fuel in 3F, then you either don’t want to see it, or simply cannot read reports.
Read all three variants. The issue is pressure building up that is why alowable g increases with lower fuel load, the fix was already identified.
Anyone want a nice laugh?
The latest David Axe masterpiece, lmao:
He is truely clueless. Well, good luck to all of the Russian posters having ignore the morons quoting that article on every comment section of defense sites/forums for the next year.
but you have gone all defensive on me.
Apologies, traveling Amtrack-enough said. Don’t have laptop with me. Here:
Scroll down and read the maneuver restrictions for all three variants. Very clear that max g envelope for all is full fuel. Probably used to have more sources-I’ll check when I can.
Well make sure you use it future – I can supply you a copy of Boman if you don’t have it.
Read the above and have a great day!