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On Time, On Target – How the Small Asteroid Lander MASCOT Caught a Ride Aboard HAYABUSA-2 in 3 Years, 1 Week and 48 Hours

Grundmann, Jan Thimo und Hendrikse, Jeffrey (2015) On Time, On Target – How the Small Asteroid Lander MASCOT Caught a Ride Aboard HAYABUSA-2 in 3 Years, 1 Week and 48 Hours. 4th IAA Planetary Defense Conference – PDC 2015, 2015-04-13 - 2015-04-17, Frascati, Roma, Italy.

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Kurzfassung

Delayed only 3 days by weather, the small asteroid lander MASCOT was launched aboard the Japanese HAYABUSA2 asteroid sample-return mission on December 3 rd , 2014, 04:22 UT, within the first interplanetary launch window. Their target is the near-Earth asteroid (162173) 1999 JU 3. The fully autonomous MASCOT carries four asteroid science instruments, orientation sensors, and an uprighting/relocation mechanism within a shoebox-sized 10 kg spacecraft. Though only an instrument-sized lander, its complexity is comparable to a similarly equipped standalone spacecraft. MASCOT is a fast paced high performance project, developed under strict constraints of volume, mass, available personnel, budget, and accessible infrastructures, to a timely deadline of a celestially fixed launch date. With a model philosophy tailored 'live' at system level, it integrates a unique mix of conventional and tailored model philosophies at units level. A dynamically adapted test programme using Concurrent Assembly Integration and Verification (Concurrent-AIV) kept project risks within acceptable bounds and shortened the system-level AIV phase from the typical 4 to 5 year to 2½ years within a project timeline of 3 years focused on the specific launch opportunity. Here, MASCOT benefited from a preceding phase of a range of lander concept studies at the DLR Bremen Concurrent Engineering Facility since 2008. Within the 3 years project timeline, from the first integrated breadboard model (½ year after first unit-level hardware breadboarding) the MASCOT team has successfully completed approx. 30 MASCOT system level tests, more than 50 additional subunit tests (excluding payloads) as well as approx. 10 test campaigns on its carrier satellite HAYABUSA2. This culminates in almost 100 different test campaigns performed in roughly half the time allocated for such a prototype project which would have followed a standardized way. MASCOT provided useful lessons in assembly, integration, testing and its related management that could be applied to increase the efficiency and decrease the lead time of future interplanetary projects from concept to launch. These lessons may become vital when the first sizeable Earth-impacting asteroid is discovered before its terminal dive. Currently, the MASCOT Flight Spare is planned to be used as Ground Reference Model and to continue functional and environmental testing on system level.

elib-URL des Eintrags:https://elib.dlr.de/97111/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:On Time, On Target – How the Small Asteroid Lander MASCOT Caught a Ride Aboard HAYABUSA-2 in 3 Years, 1 Week and 48 Hours
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Grundmann, Jan Thimojan.grundmann (at) dlr.dehttps://orcid.org/0000-0002-8809-0981NICHT SPEZIFIZIERT
Hendrikse, JeffreyAirbus Defense and Space (former Astrium GmbH.), Friedrichshafen, GermanyNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:April 2015
Referierte Publikation:Nein
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:MASCOT, concurrent AIV, constraints-driven design, responsive space missions, HAYABUSA2
Veranstaltungstitel:4th IAA Planetary Defense Conference – PDC 2015
Veranstaltungsort:Frascati, Roma, Italy
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:13 April 2015
Veranstaltungsende:17 April 2015
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Erforschung des Weltraums
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R EW - Erforschung des Weltraums
DLR - Teilgebiet (Projekt, Vorhaben):R - Projekt MASCOT (alt)
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme
Hinterlegt von: Grimm, Christian
Hinterlegt am:09 Jul 2015 12:10
Letzte Änderung:24 Apr 2024 20:02

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