A rocket engine uses stored rocket propellants as the reaction mass for forming a high-speed propulsive jet of fluid, usually high-temperature gas. Rocket engines are reaction engines, producing thrust by ejecting mass rearward, in accordance with Newton's third law. Most rocket engines use the combustion of reactive chemicals to supply the necessary energy, but non-combusting forms such as cold gas thrusters and nuclear thermal rockets also exist. Vehicles propelled by rocket engines are commonly called rockets. Rocket vehicles carry their own oxidizer, unlike most combustion engines, so rocket engines can be used in a vacuum to propel spacecraft and ballistic missiles.Compared to other types of jet engines, rocket engines are the lightest and have the highest thrust, but are the least propellant-efficient (they have the lowest specific impulse). The ideal exhaust is hydrogen, the lightest of all elements, but chemical rockets produce a mix of heavier species, reducing the exhaust velocity.Rocket engines become more efficient at high speeds, due to the Oberth effect.
I'm a junior attending an accelerated high school who's working on this year's science project. As of right now, I'm planning on building a liquid fuel rocket that is powered by gasoline with concentrated hydrogen peroxide acting as an oxidizer. I am currently working through the equations...
Hya!
Me and my friend are planning to build a rocket for our exam project. We're pretty sure going to use some kind of solid fuel, black powder most likley. It's going to bee great. :biggrin:
Now, my question is, do anybody know if there is someone who have built and flown a small liquid...