Rotating Detonation Engines vs. Continuous Combustion: The Unique Advantages To Optimize Your Cycle Model
Every gas turbine engineer learns the Brayton cycle early in [...]
Axial Turbine Design: Small Assumptions with Big Mechanical Consequences
The design of an axial turbine—or any turbomachinery component—requires careful [...]
Multistage Radial Turbines: When to Move Beyond Single-Stage Design
Radial turbines have long occupied a unique niche in turbomachinery. [...]
Supersonic Turbines Convergent-Divergent Vaned Nozzles Losses and Deviation Models
Proceedings of ASME Turbo Expo 2025
![Fig. 2. External appearance of the turbopump unit (TPU) of a RD0120 engine [3]](https://www.softinway.com/wp-content/uploads/2025/04/TPFig2-669x272.jpg)
Joint Operation of the Turbine and Pump of a Liquid Rocket Engine
The turbopump unit (TPU) is often referred to as the [...]
System Aspects of European Reusable Staged-Combustion Rocket Engine SLME
Proceedings of the 9th Edition of the Space Propulsion Conference
The Renaissance of Hybrid Rocket Engines: Advancing Small Satellite Propulsion
Authors: Victor Yevlakhov & Maya Ambrozhevich Over the past two [...]
Hybrid Rocket Engines: Bridging the Gap Between Solid and Liquid Propulsion Systems
What is a Hybrid Rocket Engine? Hybrid rocket engines (HREs) [...]
Technology Roadmap for the Development of a European Staged Combustion Rocket Engine for Reusable Launch Vehicles
Proceedings of the 9th Edition of the 3AF International Conference on Space Propulsion | May 20-23, 2024 | Glasgow, Scotland