2. Liquid Propulsion (2)

Papers

2. Design & Development of Propellant Intake Device for Cryo Upper Stage LOX Tank

4. Investigation on flow-type coupling oscillations of the preburner sub-system of the staged combustion cycle engine

6. heat transfer and pyrolysis characteristics of methane in rocket nozzle cooling channels

7. Numerical Investigation of Subcritical Combustion in Cryogenic Rocket Engine

8. photographic investigation of impinging combustion for the hydrogen peroxide and amine-based hypergolic propellant

9. Design and development of a large stroke and high cyclic life solenoid valve for bi-propellant spacecraft thrusters

10. Computational Fluid Dynamics Model for an Additively Manufactured Liquid Bi-Propellant Coaxial Swirl Injector

11. ACTiVE use of side forces on aerospike nozzles

12. Hydraulic Model 3 Test Campaign for Verification of the Bang-Bang Pressurization System of the Orion European Service Module

13. effect of floating ring seal clearance on the performance of centrifugal pump used in liquid rocket engine

15. Efficiency of high-temperature generator pressurization systems of liquid methane LV tanks