NASA NTRS ยท 19740026132
Liquid rocket engine turbines
Abstract
Criteria for the design and development of turbines for rocket engines to meet specific performance, and installation requirements are summarized. The total design problem, and design elements are identified, and the current technology pertaining to these elements is described. Recommended practices for achieving a successful design are included.
Keep this discovery
Explore connections, maps & timelines
1974-01-01. Liquid rocket engine turbines. https://ntrs.nasa.gov/citations/19740026132
Cite the original work for its findings. Save a collection to share your selection of sources.