Dominic Freudenmann

ORCID: 0000-0003-4027-8878
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About
Contact & Profiles
Research Areas
  • Energetic Materials and Combustion
  • Rocket and propulsion systems research
  • Ionic liquids properties and applications
  • Electrohydrodynamics and Fluid Dynamics
  • Catalysis and Oxidation Reactions
  • Crystal Structures and Properties
  • Inorganic Chemistry and Materials
  • Polyoxometalates: Synthesis and Applications
  • Crystallization and Solubility Studies
  • Catalytic Processes in Materials Science
  • X-ray Diffraction in Crystallography
  • Synthesis and characterization of novel inorganic/organometallic compounds
  • Thermal and Kinetic Analysis
  • Spacecraft and Cryogenic Technologies
  • Chemical Synthesis and Reactions
  • Inorganic Fluorides and Related Compounds
  • Advanced Combustion Engine Technologies
  • Crystallography and molecular interactions
  • Semiconductor materials and devices
  • Spacecraft Design and Technology
  • biodegradable polymer synthesis and properties
  • Advanced ceramic materials synthesis
  • Mesoporous Materials and Catalysis
  • Biodiesel Production and Applications
  • Combustion and Detonation Processes

Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
2016-2024

Karlsruhe Institute of Technology
2010-2014

Ionic liquids are credited with a number of unusual properties. These include low vapor pressure, wide liquid-phase range, weakly coordinating properties, and high thermal/chemical stability. properties certainly great interest for inorganic synthesis the creation novel compounds. On other hand, repertoire preparing compounds has always been broad, ranging from syntheses in solutions melts to solid-state reactions, crystal growth gas phase high-pressure syntheses. What new aspects can ionic...

10.1002/anie.201100904 article EN Angewandte Chemie International Edition 2011-10-11

Abstract Ionischen Flüssigkeiten wird eine Reihe an ungewöhnlichen Eigenschaften zugeschrieben. Hierzu zählen geringer Dampfdruck, weiter flüssiger Existenzbereich, schwach koordinierende Eigenschaften, hohe thermisch‐chemische Stabilität – die ohne Frage für anorganische Synthese und Herstellung neuartiger anorganischer Verbindungen von großem Interesse sind. Anderseits ist das Syntheserepertoire seit jeher breit reicht Synthesen in Lösungen Schmelzen bis zu Festkörperreaktionen der...

10.1002/ange.201100904 article DE Angewandte Chemie 2011-10-11

By reaction of elemental bismuth, sulfur, bismuth(III) chloride and gallium(III) in the ionic liquid (BMIm)Cl (BMIm: 1-butyl-3-methylimidazolium), [Bi3GaS5]2[Ga3Cl10]2[GaCl4]2·S8 is obtained as red transparent crystals. According to X-ray structure analysis based on single crystals, title compound crystallizes with triclinic lattice symmetry composed heterocubane-type [Bi3GaS5]2+ cations, trimeric star-shaped [Ga3Cl10]− anions three (GaCl4) tetrahedra sharing a central chlorine atom,...

10.1039/c0dt00985g article EN Dalton Transactions 2010-11-03

Abstract This article gives a short review on compatibility and chemical stability of selected aqueous ADN HAN‐based energetic formulations. A brief introduction will outline Energetic Ionic Liquids (EILs) as new class materials with beneficial physical‐chemical properties which make them valuable for application in propulsion technologies. EILs combine the advantages e. g. low toxicity, showing equal or superior power compared to state‐of‐the‐art monopropellant hydrazine. Focus is set open...

10.1002/prep.201900127 article EN cc-by Propellants Explosives Pyrotechnics 2019-07-29

Abstract By reaction of elemental tellurium, tellurium(IV) chloride, tantalum(V) chloride and oxychloride in the ionic liquid [BMIM]Cl ([BMIM]Cl:1‐Butyl‐3‐methylimidazolium chloride),[Te 8 ] 2 [Ta 4 O Cl 16 is obtained form lucent black crystals. The title compound consists infinite [Te–Te–(Te 6 )] n 2+ chains (Te–Te: 264.9(1)–284.3(1) pm) isolated 4– anions. are interconnected to a two‐dimensional tellurium network 335.9 pm). Due this interaction [Te show an arrangement that differs...

10.1002/zaac.201100143 article EN Zeitschrift für anorganische und allgemeine Chemie 2011-07-25

Ionic liquids are promising candidates for future fuels in space propulsion. In this work, six ionic with thiocyanate anions proposed as new fuel hydrogen peroxide an oxidizer. The influence of the cation is studied by pyridinium- and pyrrolidinium-based various alkyl chains. Characterization comprises, inter alia, thermal analysis, viscosity, density measurement. Calculations theoretical performance hypergolic propellants were performed NASA Chemical Equilibrium Applications comparison...

10.1021/acs.energyfuels.1c02427 article EN Energy & Fuels 2021-09-09

Abstract Three trialkylsulfonium thiocyanate ionic liquids (ILs) are presented as fuel candidates for novel green hypergolic propellants. The physical and chemical properties such density, viscosity, melting point decomposition temperature well the enthalpy of formation ILs were determined. Further, research focused on potential components propellants with highly concentrated hydrogen peroxide oxidizer. For this, theoretical maximum specific impulses calculated NASA CEA. To evaluate ignition...

10.1002/prep.202400151 article EN cc-by-nc-nd Propellants Explosives Pyrotechnics 2024-10-14

Abstract Microencapsulated ionic liquids (ILs) have a wide range of exciting properties. They can be synthesized by variety methods, which interfacial polymerization represents very simple, fast, and reliable production process, but the number available shell materials that obtained this method is limited. However, recent advances in field described formation polyamide membrane at IL/organic phase interface, extended work to first microencapsulation ILs with shell, providing an additional...

10.1002/admi.202400393 article EN cc-by Advanced Materials Interfaces 2024-11-08

As of now, the most widely used hypergolic fuels are hydrazine derivates with nitrogen tetroxide as oxidizer. The toxicity and carcinogenic character these substances make their handling challenging even if gelled. Therefore, there is great interest throughout propulsion community in finding alternatives for substances. However, despite a thorough literature review, clear selection criteria "green" hypergols could not be found. To tackle this issue, we developed set key requirements...

10.1615/intjenergeticmaterialschemprop.2018028057 article EN International Journal of Energetic Materials and Chemical Propulsion 2018-01-01

Regarding the research on alternatives for monopropellant hydrazine, several so called green propellants are currently under investigation or qualification.Aside others, DLR Institute of Space Propulsion investigates a N 2 O/C H 4 premixed propellant.During activities, flashback from rocket combustion chamber into feeding system has been identified as major challenge when using propellant mixture.This paper shows results ignition experiments conducted in cylindrical, optical accessible...

10.17265/1934-8975/2017.12.001 article EN cc-by-nc Journal of Energy and Power Engineering 2017-12-28

Transpiration cooling systems are a promising approach to handle the high wall temperatures and heat loads generated in supersonic combustion ramjets (scramjets). The German Aerospace Center DLR has developed set up versatile test bench investigate applicability of transpiration scramjets the phenomena resulting out interaction between such system, optional shock generators like wedge shaped struts hot gas main flow. In publication at hand, its components presented detail, as well...

10.2514/6.2016-4968 article EN 52nd AIAA/SAE/ASEE Joint Propulsion Conference 2016-07-22

In recent investigations at DLR Lampoldshausen a highly active catalytically promoted ionic liquid fuel with hydrogen peroxide was found. This is based on an and dissolved metal salt as catalytic promoter. But due to high viscosity of this bad mixing behaviour between reliable ignition not achieved. investigation introduced different amounts organic solvent the drop test were conducted evaluate hypergolic performance. Repeatable achieved delay times around 28 ms.

10.13009/eucass2019-653 article EN 2019-01-01

[BMIm]4[AgMo10Cl35] is prepared by reaction of MoCl5 and elemental silver in the ionic liquid [BMIm][AlCl4] ([BMIm(+)]: 1-butyl-4-methylimidazolium). Surprisingly, oxidized under these conditions. The title compound contains a new wheel-shaped [Mo10Cl35](5-) chlorido molybdenum(iii) species with five pairs Mo-Mo bonds. distances are found to be 263 pm on average. wheels exhibit maximum opening 558 diameter. They interlinked via Ag(+) form infinite [AgMo10Cl35](4-) chains. characterized...

10.1039/c4dt01100g article EN Dalton Transactions 2014-07-30

The title compound, [Te(8)][NbOCl(4)](2), was obtained as translucent black crystals by reaction of elemental tellurium, niobium(V) chloride and oxychloride in the ionic liquid BMImCl (BMImCl is 1-butyl-3-methylimidazolium chloride). synthesis performed argon-filled glass ampoules. According to X-ray structure analysis based on single crystals, compound crystallizes with triclinic lattice symmetry consists infinite {[Te(8)](2+)}(n) cations associated pyramidal [NbOCl(4)](-) anions. novel...

10.1107/s0108270112038176 article EN Acta Crystallographica Section C Crystal Structure Communications 2012-09-21

A theoretical screening and experimental characterization of the hypergolicy different ionic liquids in combination with highly concentrated hydrogen peroxide was conducted. The aim investigation to find a possible alternative hypergolic bipropellant substitute commonly used propellant combinations hydrazines dinitrogen tetraoxide. Highly chosen as green oxidizer, were fuels. Ionic offer very low vapor pressures compared common fuels, which allows simplified handling procedures. focused on...

10.1615/intjenergeticmaterialschemprop.2019028004 article EN International Journal of Energetic Materials and Chemical Propulsion 2019-12-12

Investigations for the development of new liquid green hypergolic propellants are carried out by Propellants department DLR Lampoldshausen. One part includes testing under flowing conditions to determine ignition delay time. Therefore an injector test setup was designed and put into operation. For first tests a proven propellant consisting Block 0 highly concentrated hydrogen peroxide chosen. Drop with were conducted. The average time 20.5 ms. 2on1 impinging manufactured. minimum during 190

10.2514/6.2019-4279 article EN AIAA Propulsion and Energy 2020 Forum 2019-08-16

Abstract This work demonstrated the large potential of sputtered iridium metal for catalytic reactions shown by example decomposition hydrogen peroxide (H 2 O ) space propulsion systems. For this purpose, was coated onto Al 3 pellets a sputter process under varied parameters. Depending on previously selected parameters, obtained metal-loaded offer closed- and/or open-shell structures. Catalytic productivity these first-generation iridium-sputtered catalysts estimated in laboratory...

10.1007/s10853-021-05897-z article EN cc-by Journal of Materials Science 2021-03-01

The German Aerospace Center’s Institute of Space Propulsion in Lampoldshausen has more than a decade experience green propellant research and propulsion hardware development for in-orbit applications. In the frame internal projects, ESA third-party projects DLR researcher gained deep extensive knowledge on associated systems, technologies. Currently, several promising technologies are investigated developed parallel, namely HyNOx mono- bipropellant technology, based nitrous oxide hydrocarbon...

10.2514/6.2024-1789 article EN AIAA SCITECH 2022 Forum 2024-01-04

For the development of advanced materials and structures with improved corrosion abrasion resistance, a better understanding complex multiphase flow/structure interaction is necessary. Besides appropriate material ceramic matrix composites (CMC) concerning harsh application conditions, precise characterization respect to compatibility relevant fuels on aging aspects and, especially, performance application-related combustion tests for ramjet scramjet propulsion are special interest. In order...

10.1615/intjenergeticmaterialschemprop.2024052411 article EN International Journal of Energetic Materials and Chemical Propulsion 2024-01-01
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