"It was evident from the start that 3D scanning and imaging were a requirement of this job."
NASA’s most powerful liquid-fuelled rocket, powered by the F-1 engine, was originally used in the Apollo Program between 1967 and 1973, to launch Saturn V rockets into orbit. Now, 40 years later, one of the original engines has been brought out of storage to be adapted for the new Space Launch Systems (SLS) Program.
Although some blueprints of the original F-1 engine design exist, the basic drawings that were available revealed a disconnect between the original design and as-built results. As such, the only way to obtain an accurate design of the F-1 was to map it using 3D tools.
Executing on the Challenge:
With more than 400 major parts to the rocket, not including bolts and fasteners, the team at NASA’s Marshall Space Flight Center, assisted by ShapeFidelity, Inc., an engineering services consultant specializing in 3D scanning and consulting for advanced manufacturing, strategized how best to achieve their goal.
“It was evident from the start that 3D scanning and imaging were a requirement of this job,” stated Rob Black of ShapeFidelity. “While the mission was clear, the magnitude of the project was huge and not easy to estimate. We weren’t sure how many parts were involved, or if it was even possible, and the fear was that once the engine was dismantled, we would have no way to reassemble it.”
3D Scanning and Point Cloud Processing:
Using Geomagic Solutions software for reverse engineering, combined with an ATOS Triple Scan and a TRITOP system for scanning, the team created a baseline scan, or Outer Mold Line (OML) model, of the entire engine. Then they methodically removed each part, scanned them individually, and processed them into accurate 3D data with Geomagic.
The Geomagic Reverse Engineering software allows for fast and accurate cleanup of point cloud data into 3D surface models. Once each part was completed, it was positioned back into the virtual assembly model based on the TRITOP assembly survey. The completed data took 4 months of careful disassembly, scanning and cataloging to create, including the delicate ducts and flow paths, which were especially susceptible to distortion during disassembly.
By the end of the project, the team had exactly what it hoped for: an accurate definition of the F-1 engine, now in 3D, and ready to be used in CAD for analysis, flow path definition, clearances, and re-creation and manufacture the original parts using new materials.