Solid and Liquid Fuel Rocket Engines for Multi-Stage Launch Vehicles
About this design
Detailed models of solid rocket engines used as first stage or booster components in theoretical rocket families, complemented by liquid ethanol engines designed for both atmospheric and vacuum conditions. Suitable for aerospace engineering and propulsion system studies.
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The files are shared to help you get inspired and speed up your workflow. They may not be fully accurate or production-ready, so review carefully before use.
| View Name | Extension | Action |
|---|---|---|
| Design file | step | |
| Front View | webp | |
| Top View | webp | |
| Bottom View | webp | |
| Left Side View | webp | |
| Right Side View | webp | |
| Isometric View | webp |
| File Name | Action |
|---|---|
| No supporting files | |
About CAD
The CAD model comprises 252 faces, 650 edges, 404 vertices, 9 solids. Surface types include 81 planar, 52 cylindrical, 46 conical, 18 spherical, 8 toroidal, 47 other surfaces. Orientations: 148 along the X-axis, 40 along the Y-axis, 64 along the Z-axis. Model dimensions: 612.30 mm wide, 612.30 mm high, 4664.11 mm deep. Volumetric data: maximum volume of 546926431.47 mm³, minimum volume of 50276.26 mm³, average volume of 98214552.96 mm³, total volume of 883930976.60 mm³
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