A Conceptual Design Study of Single Stage Partial Admission Supersonic Turbine for Liquid Rocket Engines
AIAA SCITECH 2025 Forum
01.01.2025
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Small, two-stage, partial-admission turbine
NTRS | 1985
|Rationale for Supersonic Afterburning Rocket Engines
AIAA | 2003
|