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Low Cost Mission to Deimos

Quantius, Dominik und Päsler, Hartmut und Braukhane, Andy und Gülzow, Peter und Bauer, Waldemar und Vollhardt, Achim und Schubert, Daniel und Romberg, Oliver und Scheibe, Karsten und Hoffmann, Harald und Börner, Anko (2010) Low Cost Mission to Deimos. COSPAR 2010, 18.-25. Jul. 2010, Bremen, Germany.

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The German non-profit amateur satellite organisation AMSAT-Deutschland successfully designed, built and launched four HEO satellites in the last three decades. Now they are going to build a satellite to leave the Earth orbit based on their flight-proven P3-D satellite design. Due to energetic constraints the most suitable launch date for the planned P5-A satellite to Mars will be in 2018. To efficiently use the relatively long time gap until launch a possible prior Moon mission came into mind. In co-operation with the DLR-Institute of Space Systems in Bremen, Germany, two studies on systems level for a first P5 satellite towards Moon and a following one towards Mars have been performed. By using the DLR’s Concurrent Engineering Facility (CEF) two consistent satellite concepts were designed including mission analysis, configuration, propulsion, subsystem dimensioning, payload selection, budgeting and cost. The present paper gives an insight in the accomplished design process and the results of the performed study towards Mars. The developed Mars orbiter is designed to carry the following four main instruments besides flexible communication abilities: -multispectral line scanner for Martian cloud investigations and Deimos (and Phobos) stereo pictures during close flybys -Deimos framing camera for high resolution pictures of Deimos (and Phobos) including video mode -sensor imaging infrared spectrometer for mineralogy of Martian (also Deimos and Phobos) silicates and surface temperature measurements -radio science for research of Deimos (& Phobos) gravity, profiling of Mars ionosphere, occurrence of third meteoritic ionosphere layer; sounding of neutral atmosphere; solar corona activity This study presents a non-industrial satellite concept that could be launched as piggyback load on Ariane 5 into GTO. It promises a low cost mission into a Mars orbit that allows close approaches to Deimos and Phobos.

Dokumentart:Konferenzbeitrag (Poster)
Zusätzliche Informationen:B02-0041-10
Titel:Low Cost Mission to Deimos
AutorenInstitution oder E-Mail-Adresse der Autoren
Quantius, DominikDLR
Päsler, HartmutAMSAT DL
Braukhane, AndyDLR
Gülzow, PeterAMSAT DL
Bauer, WaldemarDLR
Vollhardt, AchimAMSAT DL
Schubert, DanielDLR
Romberg, OliverDLR
Scheibe, KarstenDLR
Hoffmann, HaraldDLR
Börner, AnkoDLR
Datum:23 Juli 2010
Referierte Publikation:Nein
Stichwörter:DLR, AMSAT, Mars, Deimos, Phobos, low cost, OPTA, DFC, MARTIS, radio amateur, CEF
Veranstaltungstitel:COSPAR 2010
Veranstaltungsort:Bremen, Germany
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:18.-25. Jul. 2010
Veranstalter :COSPAR
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Technik für Raumfahrt
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R SY - Technik für Raumfahrtsysteme
DLR - Teilgebiet (Projekt, Vorhaben):R - Systemanalyse Raumsegment
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Systemanalyse Raumsegmente
Hinterlegt von: Dominik Quantius
Hinterlegt am:23 Aug 2010 14:01
Letzte Änderung:08 Mai 2014 23:22

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