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Christian Bach

Research Associate / Lecturer

Technische Universität Dresden

Germany

Research Interests

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About

Christian Bach is a Research Associate and Lecturer at Technische Universität Dresden, Germany. His current research areas include thrust vectoring in monopropellant thrusters, nozzle performance for reusable launch vehicles, and the application of wood-based materials in space technology. He has contributed to recent articles on experimental thrust analysis, advanced nozzle interactions, and innovative ceramic composites for liquid rocket engines.

Articles (20)

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2026

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2026

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2025

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2024

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2024

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2022

Collaborators (11)

Dario Pastrone

Full Professor

Politecnico di Torino

ITALY

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Daniele Bianchi

Sapienza University of Rome

ITALY

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Tino Schmiel

Head of satellite systems and space science

Technische Universität Dresden

GERMANY

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Martin Sippel

Deutsches Zentrum für Luft- und Raumfahrt

GERMANY

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Uwe Teicher

Professor for Manufacturing and Machining Technology

Westsächsische Hochschule Zwickau

GERMANY

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Suk Min Choi

Assistant Professor

Korea Aerospace University

SOUTH KOREA

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Kostas Giannis

Technische Universität Braunschweig - Institut für Partikeltechnik - Center of Pharmaceutical Engineering (PVZ)

GERMANY

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Andrea Ferrero

Politecnico di Torino

ITALY

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Martin Tajmar

Professor

Technische Universität Dresden

GERMANY

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Wolfgang Armbruster

GERMANY

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Jascha Wilken

Deutsches Zentrum für Luft- und Raumfahrt (DLR)

GERMANY

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Christian Bach

Research Interests

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About

Articles (20)

Identifying the Continuum Breakdown of a Plume Surface Interaction in Near Vacuum Environment for a CFD-DSMC Approach

Numerical Investigation on the Use of Plasma Actuators for Separation Control in Over-Expanded Nozzles

Simulation of the plume-surface interaction with a manufactured landing pad

RANS Simulations of Advanced Nozzle Performance and Retro-Flow Interactions for Vertical Landing of Reusable Launch Vehicles

Experimental Investigation of PWM Throttling in a 50-Newton-Class HTP Monopropellant Thruster: Analysis of Pressure Surges and Oscillations

Parametric study for the stability assessment in hydrogen peroxide monopropellant blowdown propulsion system using reduced-order models

Modeling the impact of a supersonic hot gas jet on aluminum sheets for recycling fragmentation

Numerical Analysis and Reduced-Order Modeling of a Clustered Aerospike Engine

Preliminary Design of an Additively Manufactured Aerospike Rocket Engine Utilizing Hydrogen Peroxide Transpiration Cooling

A Coupled CFD-DSMC Approach to Analyse the Plume Surface Interaction in Rarefied Conditions

Assessing the Applicability of Terrestrial Recycling Fragmentation Technologies in Lunar Conditions: A Review

Development and Testing of a 3 kN Ethanol/LOX Rocket Engine for Sounding Rocket Application

Evaluation of Hot-Fire Test Campaign of a 6 kN H2O2/Kerosene Aerospike Engine Demonstrator

From Design to Additive Manufacturing: Advancing a LOX/Methane Clustered Aerospike Engine Segment towards Experimental Velidation

Insights on the Development of the Wood-Fibre Based Thermal Protection Material TPSea

Numerical and Experimental Investigation of Lunar Landing Pad Materials for Plume-Induced Dust Mitigation

Solid Oxide Fuel Cells for Space Exploration

Surface Pressure Measurement of Truncated, Linear Aerospike Nozzles Utilising Secondary Injection for Aerodynamic Thrust Vectoring

Wood and Wood-Based Materials in Space Applications—A Literature Review of Use Cases, Challenges and Potential

Investigations on an All-Oxide Ceramic Composites Based on Al<sub>2</sub>O<sub>3</sub> Fibres and Alumina–Zirconia Matrix for Application in Liquid Rocket Engines

Collaborators (11)

Dario Pastrone

Daniele Bianchi

Tino Schmiel

Martin Sippel

Uwe Teicher

Suk Min Choi

Kostas Giannis

Andrea Ferrero

Martin Tajmar

Wolfgang Armbruster

Jascha Wilken

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