Fittings and adapters
Liquid Rocket Engine Nozzle (Sea-Level Test)
- Bounding box
- 86.0 × 86.0 × 133.8 mm
- Engine
- Precision B-rep
- Parameters
- 12
- Published
- October 13, 2026
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The prompt
make a liquid engine nozzle for rocket best for testing purpose on earth
Parameters
| Name | Value | Range |
|---|---|---|
| Chamber Diameter | 44 mm | 10 – 120 |
| Cylindrical Chamber Length | 40 mm | 5 – 150 |
| Convergent Half Angle | 30 deg | 15 – 60 |
| Throat Diameter | 16 mm | 3 – 60 |
| Divergent Half Angle | 15 deg | 5 – 40 |
| Nozzle Exit Diameter | 50 mm | 5 – 200 |
| Wall Thickness | 3 mm | 1 – 12 |
| Mounting Flange OD | 86 mm | 20 – 220 |
| Flange Thickness | 6 mm | 2 – 25 |
| Bolt Circle Diameter | 70 mm | 10 – 200 |
| Bolt Hole Diameter | 6.6 mm | 2 – 20 |
| Bolt Hole Count | 6 count | 3 – 16 |
Every value above is a live dimension. Open a model like this in the editor and each one becomes a slider you can drag before exporting.
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