3D preview of Sounding rocket cfd fea
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Interactive 3D model of Sounding rocket cfd fea

Brackets and mounts

Sounding rocket cfd fea

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Bounding box
260 × 259.9 × 2641 mm
Engine
Robotics B-rep
Parameters
12
Published
November 9, 2026

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The prompt

Model a sounding rocket for CFD analysis and FEA analysis with the following parameters: Nose Cone: A von Karman nose (i.e., the Haack series with shape parameter = 0). Length of the nose = 715 mm Radius of the nose = 130 mm Wall thickness = 3 mm Cylindrical Body Tube: length = 1785 mm radius = 130 mm wall thickness = 2 mm Solid Fuel Motor (Mounted inside the body tube): length = 1000 mm radius = 120 mm CD-Nozzle (Mounted at the extreme end of the rocket): inlet diameter = 120 mm (connected to the motor) throat diameter= 3 mm throat length = 1 mm exit diameter = 80 mm convergence and divergence half angles are 30, 45 degrees. do not model the fins, i will model them accordinlgy

Parameters

NameValueRange
Nose cone length715 mm200 – 1500
Nose wall thickness3 mm1 – 10
Body tube radius130 mm40 – 400
Body tube length1785 mm300 – 4000
Body tube wall thickness2 mm1 – 10
Motor grain length1000 mm100 – 2500
Motor grain radius120 mm30 – 380
CD nozzle overall length141 mm20 – 400
Nozzle inlet diameter120 mm20 – 380
Nozzle throat diameter3 mm1 – 60
Nozzle throat length1 mm0.5 – 20
Nozzle exit diameter80 mm5 – 300

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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Sounding rocket cfd fea - Free CAD Model (STEP, STL) | TextoCAD