You spent two decades solving the hardest propulsion engineering problems on the planet. The combustion chemistry behind Merlin and Raptor involves stiff ODE systems with rate constants spanning 8+ orders of magnitude -- the kind of problem that breaks most numerical methods.
I built something that solves exactly that class of problem using neural networks. And you are one of very few people who would immediately understand what the numbers below actually mean.
Physics-Informed Neural Networks (PINNs) should be able to learn stiff ODE systems directly. In practice, they fail catastrophically -- the competing loss terms from fast and slow timescales create gradient conflicts that the optimizer cannot resolve.
Every PINN paper says "future work" when it hits stiffness ratios above 10^4. I solved it.
Same network, same optimizer, same epochs, same seed. Only difference: my training modification. No architecture changes, no hyperparameters, < 3% computational overhead.
Stiff & Propulsion-Relevant Problems
| Problem | Standard PINN | My Method | Gain |
|---|---|---|---|
| Robertson Stiff ODE (stiffness 7.5 x 10^8) | 65.4% | 0.03% | 2,336x |
| Burgers Equation (viscous shock, Re~1050) | 15.8% | 0.55% | 28.7x |
| Helmholtz Equation (k^2=60) | 67.8% | 0.77% | 87.8x |
Robertson's rate constants: 0.04, 10^4, and 3 x 10^7. Standard PINNs produce output worse than a trivial guess (65.4% error). My method resolves all three species to 0.03%.
Additional Benchmarks
| Problem | Standard PINN | My Method | Gain |
|---|---|---|---|
| Poisson (k=5) | 556% | 0.22% | 2,483x |
| Poisson (k=10) | 282% | 0.04% | 6,883x |
| 2D Diffusion | 33.2% | 0.27% | 122x |
Geometric mean across all 6: 480x. The harder the problem, the larger the gain. Not tuned -- the method adapts on its own.
The Robertson stiffness ratio of 7.5 x 10^8 is comparable to what you see in hydrocarbon combustion mechanisms -- the chemistry behind every engine you have ever built. If PINNs could handle that stiffness natively, combustion modeling shifts from days of classical simulation to real-time inference.
The Burgers shock at Re~1050 captures the advection-dominated dynamics relevant to nozzle flow. Standard PINNs smear the shock entirely. My method resolves it to 0.55%.
I am not claiming this replaces Cantera tomorrow. I am saying the fundamental obstacle -- multi-scale gradient conflict in neural PDE training -- is solved. The applications follow from there.
Hardware: NVIDIA RTX PRO 6000 (96 GB VRAM), 255 GB RAM, Python 3.12, PyTorch CUDA.
Patent pending. Full technical details available under NDA.
What I have shown here is the most straightforward application of a deeper principle. The same core idea produces results in domains that have nothing to do with PDEs.
I built this alone. What I need now is a technical partner with the infrastructure to bring it to the real world. What I have shown here is significant -- but what I have not shown here is bigger.
bruce.tender@gmail.com