Brackets and mounts
Earth Observation Satellite - Cuboid Solar Array
- Bounding box
- 172.7 × 172.7 × 151.1 mm
- Engine
- Precision B-rep
- Parameters
- 14
- Published
- October 21, 2026
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The prompt
Create a new and original Earth observation satellite design. The satellite must have a cylindrical central spacecraft body. Arrange connected solar panels around the body in a three-dimensional rectangular-prism configuration, with panels facing different directions. Leave a gap between the cylindrical body and the solar panel structure. Use structural support rods to hold the panels in place. Leave an open area for the antenna. Show clearly divided solar panels, mechanical joints, mounting brackets, and structural connections. Present the design as a professional black-and-white patent-style engineering illustration with an isometric view. Do not create a torus, donut-shaped structure, or circular solar panel ring. Do not use conventional flat solar wings extending from opposite sides. Keep the central spacecraft body cylindrical, not rectangular.
Parameters
| Name | Value | Range |
|---|---|---|
| Bus Diameter | 60 mm | 30 – 140 |
| Bus Height | 90 mm | 40 – 220 |
| Nadir Sensor Diameter | 26 mm | 8 – 60 |
| Panel Cage Half-Size | 80 mm | 50 – 180 |
| Panel Cage Height | 110 mm | 50 – 260 |
| Panel Thickness | 4 mm | 1.5 – 14 |
| Panel Division Gap | 8 mm | 2 – 24 |
| Antenna Opening Width | 32 mm | 10 – 90 |
| Structural Rod Diameter | 8 mm | 3 – 22 |
| Hinge Joint Diameter | 12 mm | 4 – 26 |
| Antenna Mast Diameter | 8 mm | 3 – 24 |
| Mast Height Above Bus | 35 mm | 10 – 140 |
| Dish Diameter | 48 mm | 16 – 140 |
| Dish Depth | 12 mm | 3 – 50 |
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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