Publications

2015

• Analytical Viscous Flow Model and Test Validation of a Swirl Injector for Rocket Engine ApplicationFiore, G., Bach, C., Sieder, J. & Tajmar, M., 2015, 6th European Conference for Aeronautics and Space Sciences (EUCASS). Krakow, June 29 – July 3Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• A Numerical Method for Blast Shock Wave Analysis of Missile Launch from AircraftHeimbs, S., Ritzer, J. & Markmiller, J., 2015, In: International Journal of Aerospace Engineering. 2015, 10, 897213Research output: Contribution to journal > Research article
• Characterisation of TEGs Under Extreme Environments and Integration Efforts Onto Satellitesvon Lukowicz, M., Schmiel, T., Rosenfeld, M., Heisig, J. & Tajmar, M., 2015, In: Journal of electronic materials. 44, p. 362-370, 9 p.Electronic (full-text) versionResearch output: Contribution to journal > Research article
• Derivation of the Planck and Fine-Structure Constant from Assis’s Gravity ModelTajmar, M., 2015, In: Journal of advanced physics. 4, p. 219-221, 3 p.Electronic (full-text) versionResearch output: Contribution to journal > Research article
• Design and First Measurements of a Superconducting Gravity-Impulse-GeneratorLörincz, I. & Tajmar, M., 2015, 51st AIAA Joint Propulsion Conference. Orlando, July 27-29Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• Development and Testing of Electric and Advanced Propulsion Systems at TU DresdenTajmar, M., Bock, D., Nürmberger, F., Hock, A. & Kössling, M., 2015, Proceedings of the 64th German Aerospace Congress (DGLR). Rostock, Sept. 22-24Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• Development and Verification of a 500 N Ethanol/LOX Rocket Engine Using Oxide-Oxide Ceramic Matrix CompositesBach, C., Sieder, J., Wehner, F., Nürmberger, M., Przybilski, O. & Tajmar, M., 2015, 6th European Conference for Aeronautics and Space Sciences (EUCASS). Krakow, June 29 – July 3Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• Development of a Compact Hall Thruster in the 50-150 Watt RangeNürmberger, F., Hock, A. & Tajmar, M., 2015, 51st AIAA Joint Propulsion Conference. Orlando, July 27-29Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution
• Development of a Highly Precise Micronewton Thrust BalanceHey, F., Keller, A., Braxmaier, C., Tajmar, M., Johann, U. & Weise, D., 2015, In: IEEE transactions on plasma science. 43, p. 234-239, 6 p.Electronic (full-text) versionResearch output: Contribution to journal > Research article
• Development of a Highly Sensitive Micro-Newton Thrust Balance: Current Status and Latest ResultsHey, F., Altmann, C., Berger, M., Fitzsimons, E., Braxmaier, C., Tajmar, M., Weise, D. & 1 others, 2015, Proceedings of the 34th International Electric Propulsion Conference. Kobe, July 4-10Research output: Contribution to book/conference proceedings/anthology/report > Conference contribution