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Entwicklung von Testszenarien und Test des Antriebssystems eines Pseudosatelliten

Köberle, Sebastian (2014) Entwicklung von Testszenarien und Test des Antriebssystems eines Pseudosatelliten. Diploma. DLR-Interner Bericht. 572-2014/08.

Full text not available from this repository.

Abstract

Unmanned solar aircraft have very long duty cycles and are hence suitable for a deployment as a pseudosatellite. They have therefore the potential to close the gap between conventional aircraft (low cost, short duty cycles) and satellites (high cost, long duty cycles). The German Aerospace Center cooperates with several industry partners in the development of the unmanned solar aircraft ELHASPA as a prototype for a commercially deployable pseudosatellite. Since the entire necessary power has to be provided by solar cells, the poweroptimized operation is a crucial challenge. Therefore a method is designed to test the permanent magnet synchronous motor ILM 115x25, that serves as a propulsion drive, in altitudes between 0 and 18 km. Experiments are conducted accordingly and analyzed. The evaluation of the experiments suggests the operation of the motor at high motor temperatures. The integration of the motor should protect it from cooling influences, as far as the maximum acceptable motor temperature is not exceeded. Furthermore, the aircraft ELHASPA should fly at low altitudes and start climbing shortly before the dusk in order to gain potential energy for the flight in the night. The results make a contribution to the development of the solar aircraft ELHASPA. Additionally, the developed procedure is applicable to test motors for the suitability for the deployment in high flying solar aircraft.

Item URL in elib:https://elib.dlr.de/94534/
Document Type:Monograph (DLR-Interner Bericht, Diploma)
Title:Entwicklung von Testszenarien und Test des Antriebssystems eines Pseudosatelliten
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Köberle, SebastianUNSPECIFIEDUNSPECIFIED
Date:2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:HAPS, pseudo satellite, electrical flight, solar flight
Institution:TU München
Department:Lehrstuhl für Luftfahrtsysteme
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Technik für Raumfahrtsysteme
DLR - Research theme (Project):R - Vorhaben Weiterentwicklung Robotik - Mechatronik und Dynamik
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Robotics and Mechatronics (since 2013) > Mechatronic Components and Systems
Deposited By: Kondak, Konstantin
Deposited On:12 Jan 2015 18:38
Last Modified:12 Jan 2015 18:38

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