elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Small Spacecraft in Small Solar System Body Applications

Grundmann, Jan Thimo and Biele, Jens and Dachwald, Bernd and Grimm, Christian and Lange, Caroline and Meß, Jan-Gerd and Seefeldt, Patric and Spietz, Peter and Spröwitz, Tom and Ulamec, Stephan (2017) Small Spacecraft in Small Solar System Body Applications. In: IEEE Aerospace Conference Proceedings. 2017 IEEE Aerospace Conference, 4.-11. Mär. 2017, Big Sky, Montana, USA. DOI: 10.1109/AERO.2017.7943626 ISBN 9781509016136

[img] PDF (paper, hq print)
3MB
[img] PDF (presentation, hq print)
11MB

Official URL: http://ieeexplore.ieee.org/document/7943626/

Abstract

In the wake of the successful Philae landing on comet 67P/Churyumov-Gerasimenko and the launch of the first Mobile Asteroid Surface Scout, MASCOT, aboard the Hayabusa2 space probe to asteroid (162173) Ryugu, small spacecraft in applications related to small solar system bodies have become a topic of increasing interest. Their unique combination of efficient capabilities, resource-friendly design and inherent robustness makes them attractive as a mission element at the frontiers of exploration of the solar system by larger spacecraft as well as stand-alone low-cost approaches to open up the solar system for a broader range of interests. The operators' requirements for cutting-edge missions compatible with available launch capabilities impose significant constraints in resources, timelines, timeliness, mass and size. To create spacecraft feasible within these constraints, the mission design teams need to accept a broad range of equipment maturity levels from fresh concepts to off-the-shelf units. The resulting Constraints-Driven Engineering (CDE) environment has led to new methods which transcend traditional evenly-paced and sequential development. We evolved and extended Concurrent Design and Engineering (CD/CE) methods originally incepted for initial studies into Concurrent Assembly, Integration and Verification (CAIV). It is applied in all phases in most of our projects to achieve convergence of asynchronous subsystem maturity timelines and to match parallel tracks of integration and test campaigns. When facing such a challenge, Model-Based Systems Engineering (MBSE) supports design trades and constant configuration evolution due to unforeseen changes. Proactive change and schedule acceleration has resulted from system-level CD/CE optimization across interface boundaries by MBSE-aided CAIV.

Item URL in elib:https://elib.dlr.de/118799/
Document Type:Conference or Workshop Item (Speech)
Title:Small Spacecraft in Small Solar System Body Applications
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Grundmann, Jan ThimoJan.Grundmann (at) dlr.dehttps://orcid.org/0000-0002-8809-0981
Biele, JensDLR-Köln, jens.biele (at) dlr.deUNSPECIFIED
Dachwald, Bernddachwald (at) fh-aachen.deUNSPECIFIED
Grimm, Christianchristian.grimm (at) dlr.deUNSPECIFIED
Lange, CarolineCaroline.Lange (at) dlr.dehttps://orcid.org/0000-0002-1709-3667
Meß, Jan-GerdJan-Gerd.Mess (at) dlr.dehttps://orcid.org/0000-0002-2117-3483
Seefeldt, PatricPatric.Seefeldt (at) dlr.deUNSPECIFIED
Spietz, PeterPeter.Spietz (at) dlr.deUNSPECIFIED
Spröwitz, TomTom.Sproewitz (at) dlr.dehttps://orcid.org/0000-0001-5369-6919
Ulamec, StephanStephan.Ulamec (at) dlr.deUNSPECIFIED
Date:9 March 2017
Journal or Publication Title:IEEE Aerospace Conference Proceedings
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI :10.1109/AERO.2017.7943626
ISBN:9781509016136
Status:Published
Keywords:Philae, MASCOT, Gossamer-1, GoSolAr, MASCOT2, AIM, AIDA, solar sail, nano-lander, concurrent engineering, concurrent AIV, model-based System Engineering, constraints-driven engineering, Hayabusa2, Rosetta, Churyumov-Gerasimenko, Ryugu, 1999 JU3, AsteroidFinder, AsteroidSQUADS/iSSB
Event Title:2017 IEEE Aerospace Conference
Event Location:Big Sky, Montana, USA
Event Type:international Conference
Event Dates:4.-11. Mär. 2017
Organizer:IEEE
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 - Projekt Mascot (Bus), Proj. Entfaltungstechnologie . Solar Sail, R - Projekt ROSETTA Lander
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Systems Engineering and Project Office
Institute of Space Systems > Mechanic and Thermal Systems
Institute of Space Systems > Land and Exploration Technology
Institute of Space Systems > Avionics Systems
Space Operations and Astronaut Training > User center for space experiments (MUSC)
Deposited By: Grundmann, Jan Thimo
Deposited On:07 Feb 2018 13:03
Last Modified:31 Jul 2019 20:16

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.