Flying a thrust-vectoring rocket can be a challenge, and even more so if you stack multiple stages and a minimalist flight computer on top of it all. But [Joe Barnard] is not one to shy away from ...

In order to significantly increase the effectiveness, performance and specific impulse of future rocket engines, high combustion chamber pressures are required ... are decisive criteria for the ...

Show the forces acting on an object in a free body diagram. The arrows represent the ... Describe the motion of the rocket. Resultant force = 50 000 N – 10 000 NResultant force = 40 000 N ...

A diagram of ... with no benefits to thrust or efficiency. Unlike the experiment by the University of Central Florida, the Japanese effort involved launching an actual rocket.