Inspired by Xcor's small-scale rocket development, in particular, their "Teacart Rocket" demonstration:
I have chosen to replicate the 50 lbf, isopropyl alcohol/nitrous oxide rocket.
| Basic Design Parameters | |
| Thrust: | 50 lbf |
| Fuel: | 99% Isopropyl Alcohol |
| Oxidizer: | Nitrous Oxide |
| Chamber Pressure: | 300 psi |
| Cooling: | Water |
| Chamber Material: | Aluminum 6061-T6 |
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