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  1. re.public.polimi.it

    PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION-PLASMA THRUSTERS Carlo E.D. Riboldi1, Marco Belan1, Stefano Cacciola1, Raffaello Terenzi1, Stefano Trovato1, Davide Usuelli1 & Giuseppe Familiari1 1Department of Aerospace Science and Technology, Politecnico di Milano - via La Masa, 34 - 20156 Milano, Italy Abstract The adoption of ion-plasma thrusters on airships, representing the ...
  2. iprop-project.eu

    5 days agoA novel design technique, where an airship featuring ion-plasma thrusters is sized for a low-altitude demonstration mission has been published on ICAS 2024 "34th Congress of the International Council of the Aeronautical Sciences conference" proceedings. The research is conducted by the of the Department of Aerospace Science and Technology, Politecnico di Milano composed by Marco Belan ...
  3. iprop-project.eu

    A novel design technique for airships featuring ion-thrusters has been presented at the 34th Congress of the International Council of the Aeronautical Sciences conference # ... The proposed presentation covered a preliminary design technique, where an airship featuring ion-plasma thrusters is sized for a low-altitude demonstration mission. The ...
  4. riboldiresearch.net

    Preliminary Sizing of High-Altitude Airships Featuring Atmospheric Ionic Thrusters: An Initial Feasibility Assessment ... Preliminary Sizing of a Low-Altitude Airship Including Ion-Plasma Thrusters: 34th Congress of the International Council of the Aeronautical Sciences (ICAS2024), Florence, Italy, 9-13 Sep. 2024 ... Preliminary Sizing and ...
  5. A new preliminary design and sizing technique for low altitude airships coping with the inclusion of ion plasma thrusters on board. Preliminary sizing results will be shown for a demonstrator airship, which will be actually built in project IPROP, showing comparisons with a baseline design with conventional electric motors, and showing trend ...
  6. researchgate.net

    Sizing loop and weight optimization. from publication: PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION-PLASMA THRUSTERS | The adoption of ion-plasma thrusters on airships, representing ...
  7. ICAS - International Council of the Aeronautical Sciences

    https://www.icas.org › icas_archive › icas2024 › data › alle.htm

    preliminary sizing of a low-altitude airship including ion plasma thrusters icas2024_0758: c. villena muñoz¹, c. lawson¹, a. riaz¹, a. sharma¹; ¹cranfield university, united kingdom design of the seneca mach 1.8 supersonic airliner with multi-fidelity aerodynamic analysis for noise-optimised take-off trajectories
  8. icas.dglr.de

    PRELIMINARY STRUCTURAL DESIGN OF A HIGH ASPECT RATIO RANSPORT AIRCRAFT WITH LAMINAR WING ... SIZING AND PERFORMANCE ANALYSIS OF A MW-CLASS ELECTRIFIED AIRCRAFT PROPULSION (EAP) SYSTEM FOR A PARALLEL HYBRID TURBOPROP CONCEPT ... PRELIMINARY SIZING OF A LOW-ALTITUDE AIRSHIP INCLUDING ION PLASMA THRUSTERS C.E.D. Riboldi¹, M. Belan¹, S ...

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