ReDSHIFT: A Global Approach to Space Debris Mitigation

被引：26

作者：

Rossi, Alessandro ^{[1
]}

Colombo, Camilla ^{[2
]}

Tsiganis, Kleomenis ^{[3
]}

Beck, James ^{[4
]}

Becedas Rodriguez, Jonathan ^{[5
]}

Walker, Scott ^{[6
]}

Letterio, Federico ^{[7
]}

Dalla Vedova, Florio ^{[8
]}

Schaus, Volker ^{[9
]}

Popova, Rada ^{[10
]}

Francesconi, Alessandro ^{[11
]}

Stokes, Hedley ^{[12
]}

Schleutker, Thorn ^{[13
]}

Alessi, Elisa Maria ^{[1
]}

Schettino, Giulia ^{[1
]}

Gkolias, Ioannis ^{[2
]}

Skoulidou, Despoina K. ^{[3
]}

Holbrough, Ian ^{[4
]}

Zazzera, Franco Bernelli ^{[2
]}

Stoll, Enrico ^{[9
]}

Kim, Youngkyu ^{[10
]}

机构：

[1] CNR, IFAC, I-50019 Sesto Fiorentino, FI, Italy

[2] Politecn Milan, Dipartimento Sci & Tecnol Aerosp, I-20156 Milan, Italy

[3] Aristotle Univ Thessaloniki, Sect Astrophys Astron & Mech, Dept Phys, Thessaloniki 54006, Greece

[4] Belstead Res Ltd, Ashford TN25 4PF, Kent, England

[5] Elecnor Deimos Satellite Syst, Puertollano 13500, Spain

[6] Univ Southampton, Astronaut Res Grp, Southampton SO17 1BJ, Hants, England

[7] Deimos Space, Madrid 28760, Spain

[8] LuxSpace Sarl, L-6832 Betzdorf, Luxembourg

[9] Tech Univ Carolo Wilhemina Braunschweig, Inst Space Syst, D-38108 Braunschweig, Germany

[10] Univ Cologne, Inst Air & Space Law, D-50923 Cologne, Germany

[11] Univ Padua, Dipartimento Ingn Ind, I-35131 Padua, Italy

[12] PHS Space Ltd, Cerne Abbas DT2 7GW, England

[13] DLR German Aerosp Ctr, D-51147 Cologne, Germany

来源：

AEROSPACE | 2018年 / 5卷 / 02期

基金：

欧盟地平线“2020”;

关键词：

space debris; mitigation; astrodynamics; 3D printing;

D O I：

10.3390/aerospace5020064

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The H2020 ReDSHIFT project aims at finding passive means to mitigate the proliferation of space debris. This goal is pursued by a twofold research activity based on theoretical astrodynamics, computer simulations and the analysis of legal aspects of space debris, coupled with an experimental activity on advanced additive manufacturing (3D printing) applied to the production of a novel small satellite. Several different aspects related to the design and production of a debris compliant spacecraft are treated, including shielding, area augmentation devices for deorbiting (solar and drag sails) and design for demise. A strong testing activity, mainly based on design for demise wind tunnel experiments and hypervelocity impacts is performed as well. The main results obtained so far in the project are outlined.

引用

页数：15

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