You need to have an X inside the brackets for the vote tally software to count it as a vote.
I found an error in my Plan. Here, I have Engine Cycles written down as using 1 die, but costing 20R. However, the action only costs 10R per die. I've fixed this back to using 2 dice instead of 1. This doesn't affect the R cost of the Plan, but it does ensure we roll all 3 of our Engineering dice. I'm fairly sure I originally intended this to use 2 dice and instead accidentally only had the R cost correct.-[X] Engineering (3 dice, +6 Bonus to All)
--[X] Conduct Design Studies (Platform) (Heavy Sounding Rocket) [AERO] 1 die 5R 0/80 30%
--[X] Engine Cycles (Tech) [MATSCI, CHEM, PROP] 1 die 20R 0/250 (1/3.5 dice median chance)
I disagree with you both. Hydrolox is easier to procure from asteroids, sure, but it certainly isn't easier to use or store by any means. IRL with modern materials science it's extremely difficult to compress and store, which goes double for in the quest. Just look at some of the recent issues with the SLS, which are a direct result of using liquid hydrogen. This makes it extremely difficult and more importantly, dangerous, to use.
Methane is almost as abundant, easy to store, easy to use, and frankly, and easy to make. To add to it, the components to make it are also extremely abundant. Water and dry ices are everywhere in the solar system.
From a reliability perspective, Methalox is the way to go.
The thing is, I just dont see the advantage of Hydrolox over methalox. Sure, it's dirt easy to get. Just hydrolysis. But it's so much harder to use in every respect. It's not as dense, it's hilariously volatile, it's not a great regenerating agent.I think you're overstating some of the issues with liquid hydrogen - the deficiencies of SLS for instance probably has more to do with mismanagement from on high. Centaur for instance is one of the best second stages in the industry today and it runs on hydrolox. Falcon-Centaur would has been a killer combo for instance.
Hydrogen is definitely more difficult to handle, but that's ok, we don't have to beeline for it. Kerolox will serve us just fine for now, and as we start getting close and closer to re-usability (through things like engine recovery and then first stage recovery) we can switch to kerosol (kerosene solvent, a highly refined form of kerosene that's used to clean microchips and won't coke and polymerize a rocket engine).
Hydrolox is a medium to long term propellant for us to break into IMO. And if we're already doing depot type missions, then we can figure out long term hydrogen storage in LEO before we deploy it to long term deep space missions.
Hydrolox has a significantly higher ISP than Methalox. This is really important for upper stages on higher energy orbits, like GTO or interplanetary missions. A hydrolox upper stage like the Centaur should absolutely be one of the things to develop in about a decade in this quest.The thing is, I just dont see the advantage of Hydrolox over methalox. Sure, it's dirt easy to get. Just hydrolysis. But it's so much harder to use in every respect. It's not as dense, it's hilariously volatile, it's not a great regenerating agent.
For that matter it's not like methane is that much harder to get.
The thing is, I just dont see the advantage of Hydrolox over methalox. Sure, it's dirt easy to get. Just hydrolysis. But it's so much harder to use in every respect. It's not as dense, it's hilariously volatile, it's not a great regenerating agent.
For that matter it's not like methane is that much harder to get.
I'm not disputing that, but that is entirely offset by the issues of fuel density. You need much more rocket to hold enough hydrogen to make any of that worth it.Mass.
Between higher specific impulse and lower mass, hydrogen significantly reduces how much mass you need to put into orbit for interplanetary missions.
A hydrogen upper stage is just nice.
A hydrogen third stage meant for earth departure is fantastic.
The kicker is that to get good performance out of hydrogen, you need to keep your dry mass low (insulated common bulkhead for prop tanks, lithium-magnesium alloys, etc.)
Mind you that's not necessarily a bad thing because plane companies will be very happy with all the matcsi research you're funding!
Compared to kerosene anyway, hydrogen-based upper stages easily double the throw weight of an equal-sized rocket to the moon or escape velocity. With methane the difference is presumably smaller and might be more case-by-case. But until you drive flight rates really high, and probably even then, hydrogen definitely has big advantages for launch vehicles.I'm not disputing that, but that is entirely offset by the issues of fuel density. You need much more rocket to hold enough hydrogen to make any of that worth it.
I'm not disputing that, but that is entirely offset by the issues of fuel density. You need much more rocket to hold enough hydrogen to make any of that worth it.
We have gotten out of the atmosphere, just not very far.Maximum possible bonuses. Neat.
Poor PHYS tag, still all alone with no bonuses.
CREW gets a pass on account of we can't even get a rocket out of the atmosphere, much less put a person in one.