Is there no simple anymore? Plane A went this far on 5 dollars electricity. Plane B went the same distance on X dollars worth of jet fuel. I want to know the distance travelled and I want to know what "X" is.
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Well, the data we do have is that the flight was just under 30 minutes and very likely under 100 miles.
From the Wikipedia on airline fuel efficiency:
The worst-performing flights are short trips of from 500 to 1500 kilometers because the fuel used for takeoff is relatively large compared to the amount expended in the cruise segment, and because less fuel-efficient regional jets are typically used on shorter flights.
In the example values table, the most efficient plane for a 560km trip burns 0.92 kg of fuel per km, so doing some rough math and assuming the electric plane travelled 100 miles, that would be roughly 148kg of fuel, or 50 gallons (190L).
At current jet fuel prices ( $3.76/gallon ) that's about $188 US in jet fuel as a rough estimate. It's unclear if the test flight went up to full altitude or if the plane was at full weight, so a fair comparison might have used even half as much jet fuel.
Edit: From some of the other comments, it seems like they might have only considered flight time as cruising time, not takeoff and landing, so my numbers will be quite far off if that's the case. My gut feeling is that this is probably the case, because this seems like too big a difference otherwise.
$5 of electricity to lift an airplane 10,000 feet definitely seems low.
If you want to be really smug, you could say a gas powered plane requires $0 of fuel to glide for 30 minutes
Now that you mention it, they specify a maximum total weight of 25,000 lbs, so at 100% efficiency it would take 339MJ of energy to lift the fully loaded plane to 10,000 ft. That can be converted as 94 kWh, and at the current cheapest electricity price in the US of $0.1235/kWh, that's $11.63
Therefore, it is literally impossible for this plane to reach 10,000 ft for $5 fully loaded.
price in the US of $0.1235/kWh, that’s $11.63
Way cheaper than I'd have guessed.
737 at max takeoff weight is 175k lbs. So that's around $80 to get airborne. Seems like a steal when you're charging easily triple that for one seat.
$5 for 30 minutes in the air. pick any speed you want. it doesn't matter. avgas and jet fuel don't compete with $5.
I pick 30 minutes at Mach 7, here's your $5 Canadian and please get out of my way, I do intend to board now.
I pick 30 minutes at Mach 7
How long do you want to spend at Mach 7 relative to stopping and starting? Because that could be a lot of G-force.
Meh just accelerate with F-force and then switch to G-force when you are up to speed and vice versa when slowing down, problem solved!
Using N-force, which is the little can of Nox under my seat
This ride is making have to P-force
Every time I hear of an all electric aircraft of any size, I always wonder what they're going to do about landing weight.
Every modern transport category jet has a higher takeoff weight than landing weight, because of the simple unavoidable fact that landings are rougher than takeoffs. Taking off, the load gradually comes off of the landing gear, on landing it's suddenly applied. Jets burn tons, literally tons, of fuel enroute, so they're considerably lighter on approach. It's why aircraft have dump valves to jettison fuel overboard in case of forced landing early in the flight.
Batteries don't get lighter as they're discharged, so...?
Batteries don’t get lighter as they’re discharged, so…?
JETTISON ZE PACKS!! PREPARE FOR LANDING!!!
The same way we make bigger aircraft with higher landing weights: beefier landing gear and structural reinforcement. Airliners don't have a lower max landing weight than takeoff because they have to, they do it because it's cheaper and more efficient. Add some more structural weight and you lose some payload, but if the efficiency gains from fuel cost savings make it worthwhile, then manufacturers will make them.
You can rethink the engineering with electric motors.
The planes you are describing are designed assuming they will be lighter on landing because of fuel. So why design them for take off weight?
Electric motors are condusive of blown wing design for example, and would have a unique landing profile. (The plane can land at much slower velocity)
Edit: yeah they've moved the engine shroud which allows for lower speeds. Given the same runway you would be able to trim vertical speed.
That ain't gonna happen on a civilian airliner.
Blown wings are basically powered lift. You're planning on bringing a civilian passenger plane down final approach at a speed it can't glide at if the power plant fails?
I could see that for a carrier based aircraft where STOL is a factor but no you're not doing that in airline operations.
Fun fact, batteries DO become lighter when they discharge. But obviously not like fuel. But it's still a fun fact.
This article is idiotic.
$5 cost. 25,000 pounds. BUT OVER WHAT FUCKING DISTANCE?
$5 gets me 23 miles in my Delica. It gets me 100 miles on my motorcycle. It gets me 30 miles in my Porsche 914. But the article says nothing about distance.
Literally the first sentence:
The first flight of the largest battery-electric aircraft to take to the skies lasted nearly half an hour while costing just $5 of electricity.
Can your Porsche 914 fly for half an hour on $5 of fuel ?
Off a cliff yeah
It would have to be a very high cliff.
Or have a really strong updraft
Or go through the center of gravity so it eventually turns back around
i just got back from a week in bali. we rent a mini ev 2 person car to get around and in the span for the whole trip we literally spend $0 because we charge them off the wall plug of the villa we stay at
but if we want to be pedantic the car is Wuling airev and iirc it has 17 kwh of battery. that is quite enough for us for the whole week, we only need to charge it once at 60%. so lets say its around 7 kwh. in Indonesia a kwh cost around $0.1. so for a whole week it only need less than a dollar for 'gas'
I did my best to find any technical data about the flight. Couldn’t find any actual numbers. FWIW it’s not intended to be a standalone method of powering the aircraft for commercial use; they plan on making it a hybrid, which makes far more sense as far as range and payload are concerned. Best guess a 25000 lb aircraft like this will probably cruise around 120-150Kt at a nice, slow, efficient airspeed for a test like this. So maybe a 40-50 mile flight because “air time” probably started as soon as they lifted off.