Enclosures and housings
155 mm Ram-Air Shell with Spinal Rod Rotor
- Bounding box
- 155.4 × 155.3 × 780.2 mm
- Engine
- Precision B-rep
- Parameters
- 22
- Published
- October 11, 2026
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The prompt
155mm NATO Artillery Shell, which has hollow inner section that contians a spinal rod around which a screw capale of drilling through air is fit to be able to spin around with incoming air, to ensure air comes there are 2 semicricel gaps in the front of the shell that have horizontal to vertical posturing to enable air to pass htrough and there is are 3d circular gap ring in the back of th shell for ht air to exit with pressure
Parameters
| Name | Value | Range |
|---|---|---|
| Shell Outside Diameter | 155 mm | 60 – 320 |
| Cylindrical Body Length | 600 mm | 200 – 1200 |
| Nose (Taper) Length | 180 mm | 40 – 500 |
| Nose Tip Diameter | 30 mm | 6 – 100 |
| Shell Wall Thickness | 20 mm | 5 – 40 |
| Base Plate Thickness | 25 mm | 8 – 80 |
| Solid Nose Tip Length | 40 mm | 10 – 200 |
| Spinal Rod Diameter | 16 mm | 6 – 40 |
| Spinal Rod Length | 700 mm | 100 – 1000 |
| Rotor Flight Count | 10 pcs | 2 – 24 |
| Rotor Flight Span | 99 mm | 20 – 105 |
| Rotor Flight Thickness | 4 mm | 1 – 12 |
| Rotor Flight Chord | 12 mm | 3 – 40 |
| Rotor Flight Pitch | 20 deg | 0 – 60 |
| Rotor Flight Spacing | 50 mm | 10 – 200 |
| Intake Gap Radius | 25 mm | 5 – 45 |
| Intake Gap Length | 60 mm | 10 – 120 |
| Intake Position (from base) | 560 mm | 40 – 1000 |
| Intake Posture (0=horiz, 90=vert) | 0 deg | 0 – 90 |
| Rear Exit Port Diameter | 12 mm | 4 – 30 |
| Rear Exit Port Count | 8 pcs | 3 – 24 |
| Rear Exit Ring Radius | 40 mm | 12 – 70 |
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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