Senior Propulsion Engineer - Combustion Devices (m/f/d)

<p><strong>Mission Brief </strong></p> <p><span class="TextRun SCXW185765873 BCX0" lang="EN-US" data-contrast="none"><span class="NormalTextRun SCXW185765873 BCX0">You will be a senior technical contributor within Combustion Devices, responsible for high-fidelity combustion CFD and the physical understanding </span><span class="NormalTextRun SCXW185765873 BCX0">required</span><span class="NormalTextRun SCXW185765873 BCX0"> to design, </span><span class="NormalTextRun SCXW185765873 BCX0">assess</span><span class="NormalTextRun SCXW185765873 BCX0"> and mature liquid rocket engine combustion hardware. You will apply reactive-flow simulation, combustion </span><span class="NormalTextRun SCXW185765873 BCX0">fundamentals</span><span class="NormalTextRun SCXW185765873 BCX0"> and test correlation to injectors, </span><span class="NormalTextRun SpellingErrorV2Themed SCXW185765873 BCX0">preburners</span><span class="NormalTextRun SCXW185765873 BCX0">, gas generators, ignition </span><span class="NormalTextRun SCXW185765873 BCX0">systems</span><span class="NormalTextRun SCXW185765873 BCX0"> and main combustion chambers, ensuring that designs are performant, stable, thermally </span><span class="NormalTextRun SCXW185765873 BCX0">robust</span><span class="NormalTextRun SCXW185765873 BCX0"> and ready for manufacture and hot-fire testing.</span></span><span class="EOP Selected SCXW185765873 BCX0" data-ccp-props="{"201341983":0,"335551550":6,"335551620":6,"335559740":360}"> </span></p> <p>Your Role in Our Space Mission: </p> <ul> <li><span data-contrast="none">Own and execute CFD analyses of reacting flows in liquid rocket engine combustion devices, from model definition and meshing through solution, verification, validation and technical recommendation.</span><span data-ccp-props="{"201341983":0,"335559740":240}"> </span></li> <li><span data-contrast="auto">Develop and apply </span><span data-contrast="none">premixed</span><span data-contrast="auto">, partially premixed and non-premixed combustion models for rocket-relevant propellant systems and operating conditions.</span><span data-ccp-props="{"201341983":0,"335559740":240}"> </span></li> <li><span data-contrast="none">Perform steady and transient RANS/URANS and, where justified, scale-resolving simulations such as LES to investigate mixing, ignition, flame stabilisation, combustion efficiency and unsteady heat release.</span><span data-ccp-props="{"20134