Paper #54410

Paper information

Paper code: IAC-19,C4,10,x54410
Room: 143A
Title: Development of re-usable liquid propulsion rocket engines (LOX / LNG) based on turbo pump fed transpiration cooled, ceramic thrust chambers
abstract: View PDF
Session: 10. Propulsion Technology (3)
symposium: C4. IAF SPACE PROPULSION SYMPOSIUM
congress: IAC-19
Type of presentation: none