That looks very cool, however I can't imagine 800w nominal output being very useful for much of anything. It needs some serious development to be practical.
That looks very cool, however I can't imagine 800w nominal output being very useful for much of anything. It needs some serious development to be practical.
You mean SpaceX uses methane?Big Tea wrote: ↑25 Aug 2022, 23:15The latest generation of Space vehicles use Methane, mostly because of the density difference with Hydrogen, plus the amount of cooling needed, and pressure. Is it likely any F1 teams would look at it? (produced by solar so 'green')mzso wrote: ↑25 Aug 2022, 22:42Well, yeah. But it's workable. I'm more skeptical about safety viability. A 750 bar tank bursting would be quite an explosion.Cold Fussion wrote: ↑19 Aug 2022, 21:06
The problem is the volumetric density is appalling. Hydrogen at 750 bar is ~42kg/m3, so if they need roughly 110kg of fuel to complete a race now, they would need roughly 34kg of hydrogen for a fuel cell with a 60% efficiency vs a 50% efficiency PU currently, which means you need a roughly 800L tank of hydrogen to complete the race, which would be a packaging nightmare.
Race fuel allowance?Tommy Cookers wrote: ↑25 Aug 2022, 16:16my (first 2) suggestions above - can someone explain what would stop them working ?
Its mostly due to long term wanting to produce fuel from atmosphere (mars) and sun power, but partly because of much less weight and bulk of the tanks needed. Also stores at -160 oddwuzak wrote: ↑26 Aug 2022, 05:22You mean SpaceX uses methane?
SLS uses liquid hydrogen for the main stage and solid rocket boosters.
I would think the main reason to use Methane is cost.
SLS uses rehashed Space Shuttle main engines (RS-25) which means they have to use liquid H2. NASA are paying something around $100m per engine which is a lot of money - $400m per flight - to just throw away but then each launch costs something like $2bn. Very old-school thinking, sadly, but they are using the usual suspects like Boeing who just always charge a fortune and just do the "same old same old".
The Blue origin RB4 engine also uses it and there are a couple of other companies intending to use RB4Just_a_fan wrote: ↑26 Aug 2022, 14:07SLS uses rehashed Space Shuttle main engines (RS-25) which means they have to use liquid H2. NASA are paying something around $100m per engine which is a lot of money - $400m per flight - to just throw away but then each launch costs something like $2bn. Very old-school thinking, sadly, but they are using the usual suspects like Boeing who just always charge a fortune and just do the "same old same old".
. . . where possible the "throttle" would reduce output to the wheels by loading the guk and charging the es. This would have the benefit of eliminating lag - the turbo is at full boost with ice charging es at 350 kW. Application of full throttle could increase output to the tyres by 700 kW without any change in ice output.Tommy Cookers wrote: ↑25 Aug 2022, 14:32. . . . In principle couldn't a 'throttle' reduce air drawn by the compressor without causing the usual 'throttling' loss of power ?
How much will the race fuel restriction impact that?gruntguru wrote: ↑27 Aug 2022, 01:02. . . where possible the "throttle" would reduce output to the wheels by loading the guk and charging the es. This would have the benefit of eliminating lag - the turbo is at full boost with ice charging es at 350 kW. Application of full throttle could increase output to the tyres by 700 kW without any change in ice output.Tommy Cookers wrote: ↑25 Aug 2022, 14:32. . . . In principle couldn't a 'throttle' reduce air drawn by the compressor without causing the usual 'throttling' loss of power ?
I think this is sort of what you were getting at.
Think more in terms of per lap energy budget. The ES permits greater flexibility in the timing of the conversion between fuel energy and mechanical energy. Doing things like improve drivability is an important part of maximising the ruleset to improve lap time
2 points there -
2026 PU Regs
5.4.6 The electrical DC power of the ERS-K may not exceed 350kW.
5.4.7 Additionally, the electrical DC power of the ERS-K used to propel the car may not exceed: • P(kW)=1850-5* car speed (kph) when the car speed is below 340kph
• 150kW when the car speed is equal to or above 340kph
5.4.8 The difference between the maximum and the minimum state of charge of the ES may not exceed 4MJ at any time the car is on the track.
5.4.9 The energy harvested by the ERS-K in each lap must not exceed 9MJ.
This limit applies to the energy going out of the CU-K and going into the ES.
5.4.10 The maximum mechanical torque of the MGU-K may not exceed 500Nm. The torque will be referenced to the crankshaft speed and a fixed efficiency correction of 0.97 will be used to monitor the maximum MGU-K mechanical torque.
Right, but the battery capacity is 4MJ.Red Rock Mutley wrote: ↑27 Aug 2022, 11:402 points there -
Firstly, the 4MJ is the delta between ES minimum and maximum for the session, it's not a per lap limit. Even when used all in one go, the ES can be refilled during the remainder of the lap, and used again in that lap. There is a per lap input limit, 9MJ but no limit on the output.
And BEV’s don’t need the 2 largest, hardest to package items. Seriously mate, go have a look at the specs of the latest FC tech.
First, you generalize something about fuel cells based on the plainest dumbest hydrogen fuel cell tech.djos wrote: ↑27 Aug 2022, 14:15And BEV’s don’t need the 2 largest, hardest to package items. Seriously mate, go have a look at the specs of the latest FC tech.
Eg Toyota’s latest Mirai uses the latest polymer electrolyte fuel cell with a power output of 114 kW and 330 cells. It has a Volume power density of 3 kW per litre.
That means the 114 kW fuel cell takes up around 38 litres of volume! To get 500 kW of power output, you’d need around 160 litres of fuel cells.
There is simply no scenario where you could make a decent F1 race car with the current tech. Even an LMP car would be grossly uncompetitive and they likely have room for more powerful FC stacks etc.