Estimate runway ground-roll requirements with transparent constant-acceleration models. Use measured POH data for real operations; this tool is for concept checks and classroom sensitivity studies.
Takeoff roll
203 m
required 233 m
Landing roll
141 m
required 235 m
Takeoff margin
667 m
74.1% available
Landing margin
665 m
73.9% available
Ground roll follows \(s = V^2 / 2a\), so a small increase in liftoff or touchdown speed produces a larger increase in distance.
This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.
Open source: review the implementation and see how the results are produced.
Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.
Estimate runway ground-roll requirements with transparent constant-acceleration models. Use measured POH data for real operations; this tool is for concept checks and classroom sensitivity studies.
Takeoff roll
203 m
required 233 m
Landing roll
141 m
required 235 m
Takeoff margin
667 m
74.1% available
Landing margin
665 m
73.9% available
Ground roll follows \(s = V^2 / 2a\), so a small increase in liftoff or touchdown speed produces a larger increase in distance.
This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.
Open source: review the implementation and see how the results are produced.
Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.