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	1	Experimental and Theoretical Investigations of the Physical Processes Related to the Retention Capability of a Double Screen Element against Liquid Hydrogen in Earth's Gravity and in Microgravity with Respect to the Applied Stimuli Pingel, André. - Göttingen : Cuvillier Verlag, 2022, 1. Auflage
	2	Design and Test of Resonance Ignition Systems for Methane/Oxygen In-Space Propulsion Systems Bauer, Christian Anton. - München : Verlag Dr. Hut, 2021
	3	Fluidic Nozzle Throats in Solid Rocket Motors Xie, Kan. - Singapore : Springer Singapore, 2019, 1st edition 2019
	4	Investigation on Heat Transfer and Injector Design Criteria for Methane/Oxygen Rocket Combustion Chambers Silvestri, Simona. - München : Verlag Dr. Hut, 2019
	5	Future Spacecraft Propulsion Systems and Integration Bruno, Claudio. - Berlin, Heidelberg : Springer Berlin Heidelberg, 2018, 3rd edition 2018
	6	Nonlinear Aeroacoustic Characterization of Resonators Förner, Kilian H.. - München : Verlag Dr. Hut, 2017
	7	Nonlinear Aeroacoustic Characterization of Resonators Förner, Kilian H.. - München : Universitätsbibliothek der TU München, 2017
	8	Computation of the Thermoacoustic Driving Capability of Rocket Engine Flames with Detailed Chemistry Török, Attila Lehel. - München : Verlag Dr. Hut, 2016
	9	Radiation from High Pressure Hydrogen-Oxygen Flames and its Use in Assessing Rocket Combustion Instability Fiala, Thomas. - München : Universitätsbibliothek der TU München, 2015
	10	Radiation from High Pressure Hydrogen-Oxygen Flames and its Use in Assessing Rocket Combustion Instability Fiala, Thomas. - München : Verlag Dr. Hut, 2015

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