A student researched and developed hybrid rocket motor
What's the big deal?
The purpose of a rocket is to deliver a payload to its destination somewhere off the ground - be it fireworks, an atmospheric experiment, a satellite or even humans. The rocket must be as powerful and fast as gravity and aerodynamic forces are relentless, and as reliable as the payload is valuable. The rocket goes nowhere without a motor. The science behind rocket motors, some have been known to say, is the very heart of rocket science itself.
Rocket motors 101
There are three main categories of rocket motors: liquid, solid and hybrid motors, each with their advantages and drawbacks. Liquid motors are what most larger rockets use as their main engines, such as the Space Shuttle, Soyuz/Proton or Falcon 9. They mix two liquid or gaseous propellants in a burn chamber in order to produce thrust, which makes for some interesting challenges with plumbing and flow control. Solid rocket motors are what you find in fireworks, or indeed as “booster” stages for the Space Shuttle or upcoming SLS - they are the white cylinders you can see strapped to the sides. Here, the propellant is designed so that you need only add a bit of sparks and you’ll be on your way. There’s no off switch, you better make sure you’re aiming in the right direction before igniting it!
At Propulse NTNU, we are designing and building a hybrid rocket motor. The idea is to fuse the relative simplicity of a solid motor with the safety and sophistication of a liquid one. We do this by having one liquid propellant component stored in a tank, and injecting it into a burn chamber filled with a solid component. As you may recall from various safety courses, a fire needs heat, an oxygen source and a fuel in order to thrive. Usually, as is the case with our motor as well, the liquid is the “oxidizer” and the solid component is the fuel. The hybrid concept is not a new one, but it is only lately that it has started to become popular outside of amateur rocketry with appliances such as atmospheric research and cubesat-sized payloads to LEO. Our motor runs on a mix of nitrous oxide (N2O) and paraffin wax. When heated, the N2O decomposes exothermically into N2 and O2, and the O2 reacts with the paraffin to make a good, old-fashioned fire. Said fire is directed out through the nozzle at the bottom, and there you have it - a rocket motor.
Why should I join?
We still have a lot of challenges to overcome. Our system needs to be light enough to lift a rocket, but robust enough to withstand temperatures of 2000 degrees C and pressures of 60 Bar. It needs to be controlled and timed accurately, and data must be collected extensively with mass flow and temperature changes being the greatest challenges. In short, the motor is an optimization project involving control, fluid simulations and mechanical analysis, chemistry, pyrotechnics, and material technology in a wonderfully challenging mix. And of course, it all needs to be overseen and administered by someone creative and driven, who can push to find solutions when they so often seem to be non-existent.
Nobody has a solution to all of this, either because it hasn’t been thought of yet, or because the solution is locked inside some bunker. With us, you’ll be doing real research and get experience solving real engineering challenges. Nobody is a rocket scientist before they start building rockets, and the only things our teammates need is creativity and a willingness to learn. Are you up for the challenge?
Any questions are welcome at email@example.com.
Can't wait? Come join us right away!