Why are petrol and diesel not used as rocket fuel like kerosene ? Which properties make them unfit for use in rocket fuel ?
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2$\begingroup$ Related: Could I home-brew my own rocket fuel? $\endgroup$– called2voyage ♦Mar 24, 2014 at 18:23
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$\begingroup$ I share the same views as the others who answered this question. I think you might find this link useful- history.nasa.gov/conghand/propelnt.htm $\endgroup$– Night DragonMar 27, 2014 at 12:50
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$\begingroup$ Can't post an answer because the question is locked but this book is a great account of the development (and misadventures) of developing rocket fuels. All the answers you seek are here library.sciencemadness.org/library/books/ignition.pdf $\endgroup$– DanielNov 23, 2014 at 23:06
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1$\begingroup$ The first liquid-fueled rocket was lofted by a LOX/Gasoline engine designed by Robert Goddard $\endgroup$– Nick TMar 14, 2015 at 0:44
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1$\begingroup$ Probably because modern astronautics all started as air force programs and kerosene is more accessible than gas in the air force so had become the hydrocarbon of choice for this family of fuel. $\endgroup$– user3528438Apr 20, 2020 at 7:19
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4 Answers
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I'll try to find a source for this, but it is my understanding that in the early days of rocketry (read: 1950's, in this context), engineers tried to use jet fuel (and probably other fuels), but the way the fuel was produced led to large variations in thrust and specific impulse from test to test.
Basically, they'd fuel up the rocket engine (on a test stand), light it up and measure the thrust. Then they'd do it again, and they would get a substantially different thrust. This led to a specification called RP-1 (Rocket Propellant 1) which dictates that any fuel carrying the designation of RP-1 must have a certain level of various impurities (e.g. sulfur) and no more. This specification is tighter than specifications for jet fuel and other hydrocarbon fuels.
EDIT: The wikipedia page on RP-1 [1] gives a more detailed description of what I said, although they attribute the problems more directly to problems with cooling the engine.
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8$\begingroup$ According to John Clark in Ignition!, the problem with JP-1 and relatives is that there are multiple mixes of hydrocarbons that will meet the specs of JP-1, and rockets are rather touchy about the exact makeup of their fuels. Thus, RP-1, which specifies things like how much of which isomers of which hydrocarbons are permitted. $\endgroup$– MarkMar 25, 2014 at 4:47
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1$\begingroup$ @Mark - think there's a separate answer in there. $\endgroup$ Mar 25, 2014 at 5:04
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$\begingroup$ I wondered if there's an RP-2 specification to succeed RP-1. There is! Neato. Nice answer that led me to learn about a lot more random things as well! $\endgroup$ Apr 20, 2020 at 0:14
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Rockets work differently to internal combustion engines. It is easier to cool an engine than it is to cool a rocket, due to the scale and usage of the exothermic reactions. rockets use specific propellants that are tested for their purity. Car engines can have fuel that have some impurities because it is ignited intermittently and is used to transform chemical energy into kinetic energy. Most Rockets ignite their fuel constantly and the resulting release of force from the chemical energy pushes the rocket away from the aperture of the rocket, even in vacuums.
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Goddard's early liquid-fueled rockets starting in 1926 did use gasoline (petrol) as the fuel, because it was easy to obtain. RP-1 kerosene is just an optimization - cleaner and somewhat more efficient.
answered Oct 9, 2014 at 16:03
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Gasoline definitely has been used in rockets, along with light napthas, toluene, benzene, and other hydrocarbons that approach the specification for gasoline. As stated in other answers, the first liquid fueled rocket used it. However, Goddard's rockets were never very efficient designs.
The issue is, to a significant degree, historical: Commercial grade gasoline does not do well in rockets, and truly successful hydrocarbon rockets were first developed by militaries that wanted to run them on jet fuel. After this, RP-1 ("kerosene") and its Russian equivalent persisted as the favored fuel for hydrocarbon powered rockets, with gasoline having few advantages to justify the cost of developing a rocket and a rocket-spec version of the fuel.
You may wish to read my answer What actually is RP-1, and how is it different from any other hydrocarbon liquid fuel?, which explains a bit more about the development of RP-1. If serious rocket development had happened in the earlier time period when most military aircraft used gasoline engines, it's possible that RP-1 would be a gasoline-type fuel rather than a kerosene.
It also should be noted that gasoline is a serious fire hazard, but kerosene is much less so.
