NASA NTRS ยท 20030068079
Coupled Fluid and Structural Analysis of Pump Stages for Space Propulsion Systems
Abstract
The objective is to develop a coupled fluid/structure analysis tool for rocket turbopumps, advance hardware concepts and designs, and improve safety, reliability, and cost of space transportation.
Keep this discovery
Explore connections, maps & timelines
Hah, Chunill. 2003-08-01. Coupled Fluid and Structural Analysis of Pump Stages for Space Propulsion Systems. https://ntrs.nasa.gov/citations/20030068079
Cite the original work for its findings. Save a collection to share your selection of sources.