- #1
Jack Oswald
- 8
- 1
Hey guys,
I'm new to the forum and I have a question that has stumped several of the professors at my school. My idea is to use an electric motor with a solid rocket engine on a thrust stand to spin the exit cone. The concept would make use of centripetal force to increase the pressure of expanding gasses against the diverging cone. The spin would be precisely controlled and could allow micro adjustments of thrust in larger engines. Additionally, if enough centripetal force is created, the exit cone could be lengthened increasing thrust by means of an electric motor rather than more propellant. Please let me know if this idea is feasible and any literature that would help me find the solution.
Regards,
Jack Oswald
I'm new to the forum and I have a question that has stumped several of the professors at my school. My idea is to use an electric motor with a solid rocket engine on a thrust stand to spin the exit cone. The concept would make use of centripetal force to increase the pressure of expanding gasses against the diverging cone. The spin would be precisely controlled and could allow micro adjustments of thrust in larger engines. Additionally, if enough centripetal force is created, the exit cone could be lengthened increasing thrust by means of an electric motor rather than more propellant. Please let me know if this idea is feasible and any literature that would help me find the solution.
Regards,
Jack Oswald