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Why Fluorine Never made it as rocket fuel


RuBisCO

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  On 7/21/2018 at 3:26 AM, RuBisCO said:

Well aside for being more corrosive than LOX, deadly toxic, producing launch pad damaging hot HF gas and corrosive HF pollution, I think the biggest problem was price.

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Sane people would point out the disadvantages you're listing. But rocket scientists in general are not sane people. So you're probably right.

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Look the reason I started this thread was to try to find other reasons then the obvious "Fluorine is demonic" (which frankly anything that burns on contact with concrete is). I think I hit on a fact that any propellant with a idealize price above $1 never flies, regardless if how hard it is to handle. Red fuming nitric acid and Hydrazine derivatives are corrosive and toxic too, but way cheaper.  

Edited by RuBisCO
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It's possible to have a look at the launch price from another pov.

(typical launch failure probability) * (cost of launchpad repairing, surroundings cleaning, and health insurance)

I guess this number will make fluorine much more expensive than fluorine market price itself.

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  On 7/22/2018 at 8:13 PM, RuBisCO said:

Look the reason I started this thread was to try to find other reasons then the obvious "Fluorine is demonic" (which frankly anything the burns on contact with concrete is). I think I hit on a fact that any propellant with a idealize price above $1 never flies, regardless if how hard it is to handle. Red fuming nitric acid and Hydrazine derivatives are corrosive and toxic too, but way cheaper.  

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Hydrazine is also storable at room temprature who is very nice in many settings. Long term storage is pretty much an requirement for missiles who many orbital rockets derive from. 
Simply having a bit better performance is often not enough if it make handling much harder.
Hydrogen is not standard propellant even if it has best performance simply because low density and very low temperature requirements.  

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  On 7/22/2018 at 8:13 PM, RuBisCO said:

Look the reason I started this thread was to try to find other reasons then the obvious "Fluorine is demonic" (which frankly anything the burns on contact with concrete is). I think I hit on a fact that any propellant with a idealize price above $1 never flies, regardless if how hard it is to handle. Red fuming nitric acid and Hydrazine derivatives are corrosive and toxic too, but way cheaper.  

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Yes. But you have to consider why that price is so high in the first place. 

It's probably hard to create, but storing it and transporting it is also immensely difficult. 

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  On 7/23/2018 at 5:28 AM, magnemoe said:

Hydrazine is also storable at room temprature who is very nice in many settings. Long term storage is pretty much an requirement for missiles who many orbital rockets derive from. 
Simply having a bit better performance is often not enough if it make handling much harder.
Hydrogen is not standard propellant even if it has best performance simply because low density and very low temperature requirements.  

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This could be said of Chlorine tri/pentafluoride, room temp storable, improves performance and density, but the cost of it is too much. 

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They were suggesting fluorine upper stages more than once. For Spiral, UR-700, etc.
This is not hundreds tons, usually just a ton or several. This doesn't cost a lot. But was rejected.

So, probably the only reason is  that even more expensive than fluorine itself are the fluorine's consequences.

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  On 7/23/2018 at 2:51 PM, kerbiloid said:

So, probably the only reason is  that even more expensive than fluorine itself are the fluorine's consequences.

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Just imagine this: 

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or this: 

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And figure out all that fluorine being spilled around...

Edited by Lisias
whoops.
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It strengthens teeth and burns everything in fire.
And it's toxic. And corrosive. And cryogenic.

So, not only that fluorine itself costs much, but if when a rocket bursts, a lot of money would be spent on the launchpad repair.
If it doesn't burst, a lot of money should be spent on precautions.

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And in fluorine atmosphere burns everything including air.

Edited by kerbiloid
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  On 7/22/2018 at 8:13 PM, RuBisCO said:

Look the reason I started this thread was to try to find other reasons then the obvious "Fluorine is demonic" (which frankly anything that burns on contact with concrete is). I think I hit on a fact that any propellant with a idealize price above $1 never flies, regardless if how hard it is to handle. Red fuming nitric acid and Hydrazine derivatives are corrosive and toxic too, but way cheaper.  

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Okay. Lets look at the numbers then.

From this site (feel free to provide an alternative), the Block 2 Falcon 9 contained a total of 174,000 litres of LOX. Liquid fluorine has a density of 1.5 kg/l. So, assuming that the Falcon 9 used 100% fluorine as an oxidiser it would need 261,000 kg of fluorine. From your price of 6$ per kilogram, that works out at $1.56m to fill a Falcon 9. Not cheap by any means but still a single digit percentage of the quoted launch price (whichever launch price you choose to use). And that's with one of the cheapest, if not the cheapest launch vehicle in its class. 

I'm sure price is a factor but it's a fairly insignificant one in the overall scheme of building and flying a launch vehicle. The obvious "Fluorine is demonic" reasons are far more compelling.

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  On 7/23/2018 at 6:17 PM, KSK said:

Okay. Lets look at the numbers then.

From this site (feel free to provide an alternative), the Block 2 Falcon 9 contained a total of 174,000 litres of LOX. Liquid fluorine has a density of 1.5 kg/l. So, assuming that the Falcon 9 used 100% fluorine as an oxidiser it would need 261,000 kg of fluorine. From your price of 6$ per kilogram, that works out at $1.56m to fill a Falcon 9. Not cheap by any means but still a single digit percentage of the quoted launch price (whichever launch price you choose to use). And that's with one of the cheapest, if not the cheapest launch vehicle in its class. 

I'm sure price is a factor but it's a fairly insignificant one in the overall scheme of building and flying a launch vehicle. The obvious "Fluorine is demonic" reasons are far more compelling.

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I actually calculated those numbers, on the first post of this thread. 

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  On 7/24/2018 at 1:35 AM, RuBisCO said:

I actually calculated those numbers, on the first post of this thread. 

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So you did - sorry.

I still don’t think that price is a particularly relevant factor here though. Until fairly recently, rocketry has not been a particularly price sensitive business. If the risks of using fluorine had been outweighed by utility or by pure performance, it would have been used.

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