Brackets and mounts
Variant 24 Inert Aerospace Training Vehicle (Assembled)
- Bounding box
- 4070.2 × 1600.0 × 662.0 mm
- Engine
- Precision B-rep
- Parameters
- 34
- Published
- September 20, 2026
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The prompt
Create a professional university-level engineering drawing for VARIANT 24 from an aerospace engineering course assignment. The subject is an inert educational aerodynamic aerospace vehicle based on the following assignment parameters: - Variant: 24 - Type: aviation aerospace vehicle - Direction: air-to-water - Design range: 500 km - Payload designation: PBCh + SBCh - Propulsion designation from the assignment: VRD + TTRD IMPORTANT: This is an academic CAD/drafting exercise only. Treat the object as a non-functional inert training model. Do not generate or specify explosive, warhead, fuel, propulsion, guidance, control, targeting, or other functional weapon-system details. Create a clean technical drawing suitable for a university engineering assignment. DRAWING REQUIREMENTS: 1. Format: A3 horizontal. 2. Technical black-and-white drafting style. 3. Use orthographic projection. 4. Main longitudinal side view as the primary view. 5. Front view. 6. Top view. 7. Add centerlines and symmetry axes. 8. Show the major external geometric elements: - aerodynamic nose section; - main cylindrical/fuselage body; - external aerodynamic surfaces; - tail section; - mounting/interface areas represented only schematically. 9. Use a consistent engineering scale. 10. Add dimension lines for the externally visible geometric dimensions. 11. Use millimeters for dimensions. 12. Use standard engineering line weights: - visible contours: thick; - construction/extension lines: thin; - centerlines: chain thin; - hidden contours: dashed. 13. Add numbered callouts for the major external sections. 14. Add a simple longitudinal section view showing only generic inert structural zones, without internal weapon, propulsion, fuel, explosive or guidance details. 15. Add a standard engineering title block in the lower-right corner. 16. Title block should contain: - Variant 24 - Aerospace Engineering - Engineering Drawing - Scale - Sheet number - Student - Group - University 17. Make all views geometrically consistent with each other. 18. Do not create artistic rendering, photorealism, textures or colors. 19. The final result must look like a genuine university mechanical/aerospace engineering drawing rather than an illustration. OUTPUT: Generate a clean, high-resolution technical drawing with accurate projection alignment, readable dimensioning, centerlines, section indication and a properly formatted title block. Do not invent operational specifications. Where the assignment does not provide exact dimensions, use clearly marked illustrative dimensions or leave dimensions unspecified rather than presenting invented values as real specifications.
Parameters
| Name | Value | Range |
|---|---|---|
| Fuselage Length | 3000 mm | 1000 – 6000 |
| Fuselage Diameter | 200 mm | 60 – 600 |
| Shell Wall Thickness | 3 mm | 1 – 12 |
| Nose Fairing Length | 600 mm | 100 – 2000 |
| Blunt Tip Diameter | 20 mm | 5 – 80 |
| Tail Cone Length | 500 mm | 100 – 1500 |
| Tail Cone Aft Diameter | 80 mm | 20 – 190 |
| Wing Span (per side) | 800 mm | 100 – 2000 |
| Wing Root Chord | 400 mm | 50 – 1200 |
| Wing Tip Chord | 200 mm | 20 – 800 |
| Wing LE Sweep | 200 mm | 0 – 1000 |
| Wing Thickness | 8 mm | 2 – 60 |
| Wing Root LE Station | 1400 mm | 100 – 2800 |
| Vertical Fin Height | 450 mm | 50 – 1500 |
| Fin Root Chord | 350 mm | 50 – 1200 |
| Fin Tip Chord | 150 mm | 20 – 800 |
| Fin LE Sweep | 250 mm | 0 – 1000 |
| Fin Thickness | 8 mm | 2 – 60 |
| Fin Root LE Station | 2550 mm | 100 – 3400 |
| Tailplane Span (per side) | 300 mm | 50 – 1200 |
| Tailplane Root Chord | 250 mm | 50 – 900 |
| Tailplane Tip Chord | 125 mm | 20 – 600 |
| Tailplane LE Sweep | 100 mm | 0 – 600 |
| Tailplane Thickness | 6 mm | 2 – 40 |
| Tailplane Root LE Station | 2700 mm | 100 – 3400 |
| Lug Width | 60 mm | 10 – 200 |
| Lug Length | 150 mm | 20 – 500 |
| Lug Pad Thickness | 20 mm | 4 – 80 |
| Lug Station 1 | 1000 mm | 100 – 2900 |
| Lug Station 2 | 2000 mm | 100 – 2900 |
| Frame Outer Diameter | 198 mm | 40 – 600 |
| Frame Inner Diameter | 158 mm | 20 – 560 |
| Frame Axial Thickness | 5 mm | 1 – 40 |
| Frame Count | 6 - | 0 – 20 |
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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