1. Skin Laminate Stackup
8 Plies / Skin
Ply Orientation Angles
2. Honeycomb Core & Geometry
3. Flight Dynamics & Aero Environment
PASS - Fully Validated Structure
Min SF: 2.45
Flexural Rigidity (D11)
142,500 N·m
Areal Density
5.82 kg/m²
Total Dry Shell Mass
1,215 kg
Face Comp Buckling SF
2.45
Core Shear Safety SF
3.12
Acoustic Attenuation @100Hz
22.4 dB
Sandwich Cross-Section & Bending Strain Field
Acoustic Transmission Loss (TL) Spectrum (10 Hz - 10 kHz)
CLT Stiffness Sub-Matrices (A11, D11)
| Property |
11 (Axial) |
22 (Transverse) |
12 (Coupling/Shear) |
| A Extensional (N/m) |
1.28e8 |
1.10e8 |
3.45e7 |
| D Bending (N·m) |
142,500 |
128,200 |
38,100 |
Structural Proof Target: rocket-fairing-composite-structure-75