DIGITAL DATCOM

Heritage aerospace analysis reimagined for the modern web. Real-time aerodynamic calculations using algorithms that powered Apollo, Shuttle, and F-16.

⚡ WebAssembly Ready
đŸĻ€ Rust Performance
đŸ“Ļ Open Source
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Aircraft Configuration
Wing Span 35.0 ft
Wing Area 174 sq ft
Wing Sweep 0°
Horizontal Tail Size 100%
Center of Gravity 25.0% MAC
⚡ Real-Time Performance
0.0003ms
Analysis Time
10-50×
Faster Than Python
✓
WebAssembly
🌐
Browser Ready
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Real-Time Analysis Results
Aircraft Configuration Stable
✅ STABLE
CG AC Reference Line
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Static Margin
+8.5%
Distance between CG and neutral point. Positive values indicate stable configuration.
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Neutral Point
32.1% MAC
Aerodynamic center of the complete aircraft configuration.
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Stall Speed
68 mph
Minimum flight speed at current configuration and weight.
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Max Lift Coefficient
1.42
Maximum lift coefficient achievable before stall.
🏛ī¸ Heritage Algorithms in Action
These calculations use the same mathematical foundations that designed Apollo, Space Shuttle, and F-16. Originally developed in 1960s Fortran, now running in your browser with modern performance.