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Never mind that this is the 18th question to have the tag.

To the question "Would the Dragon escape pod have survived this event?" asked about the AMOS-6 mission, Elon Musk tweet-responded:

yes. This seems instant from a human perspective, but it really a fast fire, not an explosion. Dragon would have been fine.

The speed of combustion was limited by the rate at which fresh oxygen and kerosene could mix and be heated. Compare that to what happens when high explosives detonate where the reaction travels through the material at the speed of sound, and no mixing is required.

So for the purposes of this question let's say that LOX/RP-1 rockets don't explode.

Question: Have there been tests of rockets that had the potential to detonate proper? Just for an illustrative example: oxidizer and fuel thoroughly mixed but kept so cold that nothing happens until some is warmed up in a combustion chamber?

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    $\begingroup$ I think you need to disambiguate your terms a little bit more. Making a rocket explode is easy: just poke a hole in a tank. The line that I think you are drawing is between a deflagration and a detonation. And explosion can be a deflagration or a detonation, and it can even be neither of those things. $\endgroup$ Feb 12, 2021 at 12:23
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    $\begingroup$ In short: explosion = rapid increase in volume, deflagration = subsonic combustion, detonation = supersonic combustion (relative to the local speed of sound in the flame front). $\endgroup$ Feb 12, 2021 at 12:26
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    $\begingroup$ @JörgWMittag That's why "detonate" already appears in the title and twice in the body of the question. and I've already addressed the speed of sound as well. Can you give it anothre read through and let me know if there are really any ambiguities there? And if not, consider deleting the comment? Thanks! $\endgroup$
    – uhoh
    Feb 12, 2021 at 13:40
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    $\begingroup$ Will you count only successful system? John D. Clark's "Penelope" fuel was unsuccessful because it was such a good high explosive it couldn't be forced to burn normally. $\endgroup$
    – SF.
    Feb 13, 2021 at 18:34
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    $\begingroup$ Will hydrazine detonate given enough encouragement? $\endgroup$
    – Roger Wood
    Feb 13, 2021 at 21:15

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Some rockets (especially hybrids) use nitrous oxide oxidizer, which exothermically decomposes into nitrogen and oxygen and is capable of detonation. This is not just a theoretical hazard, Virgin Galactic experienced an explosion during a cold-flow injector test in 2007 that killed 3 people and injured 3 more.

Acetylene is typically handled as a solution in acetone due to it being prone to explosive decomposition in liquid form or as a high pressure gas, which can happen supersonically in a detonation. However, the DARPA ALASA program attempted to use a monopropellant consisting of a mixture of acetylene and nitrous oxide. The program was terminated in 2015 due to the propellant exploding in testing. The explosion of such a mixture seems likely to progress to detonation.

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    $\begingroup$ To "Have any rocket fuel systems actually been explosive, and could have detonated proper?" This answer seems to be "Yes, and here are two examples." Thanks! $\endgroup$
    – uhoh
    Jul 16, 2021 at 1:06
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As a rule of thumb, no rocket fuel (or oxidizer) will ever be able to detonate on its own. For the simple reason that the maximum flame front propagation through it needs to be slower than the fluid speed through the injectors, otherwise the flame would propagate back into the tanks. NO, no-one has ever managed to pump flammable fluids faster than their speed of sound.

As for the mixture? Absolutely. Even a simple beast such as the Proton rocket's mixture of unsymmetrical dimethyl hydrazine and nitrogen tetroxide will detonate, if you somehow achieve complete mixing before igniting it. This may be difficult though, as this combination is exceedingly hypergolic, and even frozen solid the materials will ignite each other.

Again, as a general rule, no. Rockets thrive on very rapid combustion, not supersonic detonations. The fuels are selected such that this is true.

P.S. Even liquid Kerosene and LOX will detonate. Quite violently, too! You just need to thoroughly mix them and emulsify the mix so the particle size is approaching zero. This just does not happen in any realistic accident or failure mode. It helps for safety that the kerosene freezes hard at a much higher temperature than the LOX boils, and liquid or solid kerosene and gaseous oxygen is very hard to mix.

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    $\begingroup$ @uhoh anyone that tried it, would have created a crater. They almost certainly did try it (although i do not recall anything from Ignition! discussing that). But with available technology, especially in early rocketry, any experiment using detonate-able premix fuel....would have detonated. In the fueltank. $\endgroup$ Feb 13, 2021 at 9:48
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    $\begingroup$ This is refuted by Clark's Ignition. They experimented with some monopropellants that could be detonated. All of them ended up having significant safety problems or other issues that led to them never finding use outside of research. $\endgroup$
    – ikrase
    Feb 14, 2021 at 7:16
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    $\begingroup$ @PcMan they got as far as testing rocket engines (and blowing up test rigs). There's little to gain by actually flying if you're just testing propellants, especially if things keep exploding. Ignition has an account of testing a monoprop they named "Penelope" where: "the reaction changed to a high order detonation which demolished the motor, propagated through the fuel line to the propellant tank, detonated the propellant there (fortunately there were only a few pounds in the tank) and wrecked just about everything in the test cell". $\endgroup$ Feb 14, 2021 at 15:26
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    $\begingroup$ @PcMan it was certainly a "test of a rocket" as specified in the final paragraph that formally states the question. The question doesn't restrict things to propellants that saw practical use. $\endgroup$ Feb 14, 2021 at 16:51
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    $\begingroup$ @PcMan are you seriously asserting that your playing around with carbonated drinks is on equal standing with rocket propellant development at the Naval Air Rocket Test Station in Dover? They dropped the propellant because it was excessively prone to detonation, not because what they were trying was fundamentally unworkable. It was tested in a real rocket engine with the intent of developing it into a propellant to be used in real spacecraft by experts in the field who had the skills and knowledge to do just that. $\endgroup$ Feb 14, 2021 at 17:10
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I think the answer is possibly yes, but the place to look is probably solid-fueled rockets not liquid-fueled ones. I am not a chemist but I believe it is the case that ammonium nitrate is used as an oxidiser in some such propellants: Wikipedia also seems to say so and says such mixtures are often known as 'ANCP'.

Well, if you do the right thing to ammonium nitrate you can make it detonate, on its own (so it's a high explosive, not a low explosive in this case). I believe that 'the right thing' is rather hard to arrange, but you definitely do not want to be trying to break up large masses of it with dynamite however.

The right thing is certainly sufficiently hard to manage that I've seen pretty substantial barns full of sacks of ammonium nitrate fertiliser: no-one worried about it exploding (people nicking it from farms and using it as an oxidiser for IEDs is another matter: I think that still goes on, unfortunately).

So I think that it's at least reasonably possible that solid-fueled rockets which use ammonium nitrate as an oxidiser are potentially using high-explosive fuels, but ones which are so hard to detonate as not to be a risk in practice. However I think that whether the thing is a high explosive depends on the concentration of ammonium nitrate, and I'm not sure what that is in rocket fuels, but it may be below the critical threshold (misjudging what the threshold was seems to have been one of the mistakes made at Oppau).

(Incidentally the speed of a detonation isn't the speed of sound in the material: it's much higher than that.)

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