DREAM CHASER FOR EUROPEAN UTILIZATION (DC4EU): ESA PILOT PHASE RESULTS
- Paper number
IAC-17,D2,4,5,x38646
- Author
Dr. Marco Berg, OHB System, Germany
- Coauthor
Ms. Andrea Jaime, OHB System AG - Munich, Germany
- Coauthor
Mrs. Antonella Sgambati, OHB System AG-Bremen, Germany
- Coauthor
Dr. Timo Stuffler, OHB System AG - Munich, Germany
- Coauthor
Mr. John Roth, Sierra Nevada Corporation, United States
- Coauthor
Dr. Luciano Saccani, Sierra Nevada Corporation, United States
- Coauthor
Ms. Kathy Benzin, Sierra Nevada Corporation, United States
- Coauthor
Mr. Neeraj Gupta, Sierra Nevada Corporation, United States
- Coauthor
Dr. Dario Castagnolo, Telespazio, Italy
- Coauthor
Mr. Franco di Stadio, Telespazio S.p.A., Italy
- Coauthor
Mr. Bernhard Hufenbach, European Space Agency (ESA), The Netherlands
- Coauthor
Mr. Marco Caporicci, European Space Agency (ESA), The Netherlands
- Year
2017
- Abstract
In 2015 ESA launched an ongoing initiative for strategic partnerships with the private sector, leveraging ideas for advancing the implementation of ESA’s space exploration strategy. A strong focus is placed on the commercial dimension of ISS utilization, post-ISS low Earth orbit exploitation and lunar exploration. In the frame of this initiative, the Dream Chaser for European Utlitization (DC4EU) has been selected by ESA for the implementation of a pilot phase. This partnership aims to establish a European on-demand low Earth orbit (LEO) operational capability using the Dream Chaser® Space Utility Vehicle developed by Sierra Nevada Corporation (SNC), a US company awarded with a NASA Commercial Resupply Services (CRS2) contract in 2016. The DC4EU service plans to offer an affordable and flexible platform for user-driven European research and technology demonstration opportunities in space. The main goals of the DC4EU service are to offer: - first class research facilities for science opportunities remain, even after the International Space Station (ISS) is decommissioned, - flight application of developed European transportation technologies (e.g. docking/berthing adapter, operational software, active debris removal, thermal protections, rendezvous and re-entry guidance navigation control, etc.) and capabilities (launch and landing) and - new technology validation in relevant environment (robotics, grappling, etc.) and generate spin-off to other areas of space activities (space exploration, in-orbit servicing, assembly in space, etc.). This paper aims to present the main results of the DC4EU pilot phase, covering a technical and programmatic feasibility assessment of the DC4EU service, description of a representative mission in LEO, the evaluation of different user scenarios and an analysis of the resources available for payloads, in terms of mass, power and communication.
- Abstract document
- Manuscript document
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