9–12 Sept 2024
University Oxford
Europe/London timezone

Test trials of the ESTHER Shock Tube

12 Sept 2024, 12:00
25m
Oxford e-Research Centre (University Oxford)

Oxford e-Research Centre

University Oxford

7 Keble Rd, Oxford OX1 3QG United Kingdom
High speed facilities, flight testing and propulsion High speed facilities, flight testing and propulsion

Speaker

Mario Lino da Silva (Instituto de Plasmas e Fusão Nuclear - Instituto Superior Tecnico)

Description

ESTHER is a two stage shock-tube. It comprises a 1.6m length and 200mm diameter combustion driver where He/H2/O2 and N2/H2/O2 mixtures are injected by an automated gas filling system at initial pressures up to 100bar. These mixtures are ignited through a Nd:Yag laser shooting on the back plate through a thick sapphire window, reaching final pressures up to 600bar for typical deflagrations (subsonic combustion). Occasionally, detonations (supersonic combustion) may occur, leading to higher transient pressures (up to 2.4kbar reflected pressures). The combustion chamber is designed accounting for such maximum pressure requirements. It is manufactured from low carbon super-duplex steel which has high mechanical strength and is tolerant for H2 presence because of minimized adsorption.

An intermediary compression tube is connected to the combustion chamber through a diaphragm designed to burst at a predetermined pressure. The compression tube is filled with He gas at pressures of about 0.01 – 1 bar. The shock-wave propagates in this section leading to transient reflected pressures of 70bar. The tube end sections are made in super-duplex stainless steel, while the middle sections are made in duplex stainless steel, which also has a low rate of Carbon, limiting adsorption. The compression tube section has an internal diameter of 130mm, and a length of about 6.5m.

The compression tube is connected to the shock-tube test section through a second diaphragm designed to burst at a predetermined pressure. The shock-tube is filled with a test gas at pressures of about 0.1 mbar. The shock-wave propagates in this section at velocities that can exceed 10 km/s, leading to transient reflected pressures of no more than 20 bar. The tube is manufactured in duplex stainless steel. The shock-tube section has an internal diameter of 80mm, and a length of about 5.9m. Pressure sensor stations are located at different stages of the shock-tube, detecting the rise of pressure in the wake of the shock-wave. This allows for developing a triggering system initiating high-speed (10 – 100 MHz rated), time-dependent spectroscopic measurements at the test-section windows (25 mm diameter) of the radiation emitted and absorbed in the wake of the shockwave.

A dump tank recovers all the gases flowing in the wake of the shock-wave. The H2O liquid phase is drained off, while the remaining contaminated He mixture is evacuated by the pumping system, after which the shock-tube can be opened for cleaning operations and the replacement of the diaphragms.

This work presents the final test-trials of the facility.

Summary

N/A

Author

Mario Lino da Silva (Instituto de Plasmas e Fusão Nuclear - Instituto Superior Tecnico)

Co-authors

Lionel Marraffa (ESA/ESTEC) Ricardo Ferreira Victor Fernandez Villace (ESA)

Presentation materials

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