The conceptual design of a CDRE (Continuous Detonation Rocket Engine) to determine viability for the commercial market.

Objective:

This projects objective is to come up with a standardised process to intially design the geomtery and performance of a conceptual CDRE, using either a Hydrogen + Air or Methane + Oxygen detonation.

Running the Code

Please find the code on Google colab

References

1: CUDA C++

2: Spesific impusle

3: CDRE injector

4: Cantera AFT

5: CDRE geometry

6: Air density

7: CH4/H2/O2 density

8: Detonation cell width ANN