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D3 SIGNED

Smart propulsive device for controlled satellite decommissioning and reentry.

Total Cost €

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EC-Contrib. €

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Partnership

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 D3 project word cloud

Explore the words cloud of the D3 project. It provides you a very rough idea of what is the project "D3" about.

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Project "D3" data sheet

The following table provides information about the project.

Coordinator
D-ORBIT SPA 

Organization address
address: VIALE RISORGIMENTO 57
city: FINO MORNASCO CO
postcode: 22037
website: n.a.

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Italy [IT]
 Project website http://www.deorbitaldevices.com
 Total cost 2˙800˙692 €
 EC max contribution 1˙960˙484 € (70%)
 Programme 1. H2020-EU.2.1.6. (INDUSTRIAL LEADERSHIP - Leadership in enabling and industrial technologies – Space)
2. H2020-EU.2.3.1. (Mainstreaming SME support, especially through a dedicated instrument)
 Code Call H2020-SMEINST-2-2015
 Funding Scheme SME-2
 Starting year 2015
 Duration (year-month-day) from 2015-12-01   to  2018-05-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    D-ORBIT SPA IT (FINO MORNASCO CO) coordinator 1˙960˙484.00

Map

 Project objective

Space is nowadays fundamental for our life. Most of the services we use every day are based on space assets: weather forecasting, navigation, Earth observation, security, disasters prevention and management, telecommunication. For decades, space faring Nations and private organisations have underestimated the fact that orbital space is a limited resource. As a consequence, out of the about 6,000 satellites launched since the beginning of the space age only 1,300 are operational: the remaining wander uncontrolled in the space around Earth and risk to collide against each other or against operational satellites. In addition to this, many dead satellites re-enter uncontrolled into the atmosphere, and their larger components survive to the high heat of the re-entry and may cause damage to assets on ground and persons. For these and other reasons, Space Operators start to develop methods to remove safely their satellites, pushed by international regulations issued by space agencies, international organisations (e.g. UN and IADC) and national governments. The D-3 project aims to respond to the increasing need to guarantee a safe and clean access to space for both satellite operators and manufacturers, and in general for all the stakeholders involved. This approach has already received positives feedbacks and endorsement from important space players such as ESA, NASA and ASI, as well as from both satellite operators and manufacturers. Since its establishment, in 2011, D-Orbit has developed a decommissioning device (called D3) for satellites and launcher stages, capable to remove them in a safe and controlled way at the end-of-mission or if a major failure occurs. This technology has been pushed up to a current TRL of 6. D-Orbit intends to validate the D-Orbit's decommissioning concept in Space in 2016 in D-SAT mission and to collect data, inputs and lessons learnt for updating, optimizing and fine tuning the design, the engineering and the production of the D-Orbit’s D3.

 Publications

year authors and title journal last update
List of publications.
2017 M. Trotti, A. Weigand, D. Alloni, L. Ferrario
Study of Radiation-Induced Effects on Inert Propellants
published pages: , ISSN: , DOI:
IAASS Conference 2017 2019-06-13
2017 Alessio Fanfani, Marco Bevilacqua, Lorenzo Ferrario, Simone Brilli, Matteo Trotti, Angelo Dainotto, Marco Cazzaniga, Francesco Palumbo, Stefano Antonetti
EOL Operations of the D-Sat Satellite: An In-Orbit Demonstration of Satellite Controlled Re-Entry
published pages: , ISSN: , DOI:
IAC 2017 2019-06-13
2017 E. Toson, M. Bevilacqua, L. Ferrario, M. Valli, P. Guerrieri
An Innovative Approach to CubeSats Dispersion: The D-Orbit ION CubeSat Carrier
published pages: , ISSN: , DOI:
IAC 2017 2019-06-13
2017 E. Toson, M. Bevilacqua, L. Ferrario, M. Valli, P. Guerrieri
D-Orbit Involvement in the ESA CleanSat Program: An Autonomous Decommissioning System for Satellite Controlled Re-Entry
published pages: , ISSN: , DOI:
IAC 2017 2019-06-13
2016 Stefano Antonetti, Elena Toson, Lesley Jane Smith, Veronica La Regina, Matteo Emanuelli
Possible Future Space Debris Mitigation and Removal Legal, Regulatory and Technical Scenarios
published pages: , ISSN: , DOI:
67th International Astronautical Congress (IAC) 2019-06-13
2016 Alessio Fanfani, Stefano Antonetti, Claudia Shekufendeh, Luca Rossettini
SATELLITE DECOMMISSIONING DEDICATED SYSTEM FOR IN-ORBIT AND ON-GROUND RISK REDUCTION
published pages: , ISSN: , DOI:
NATO AVT-257 Specialists\' Meeting Best Practices for Risk Reduction for Overall Space Systems 2019-06-13
2016 Alessio Fanfania, Simone Brilli, Matteo Trotti, Angelo Dainotto, Elena Toson, Alexander Weigand, Fabio Nichele
Launch of a 3 Unit Cubesat with integrated propulsion system: D-SAT qualification, acceptance and transportation logistics
published pages: , ISSN: , DOI:
67th International Astronautical Congress (IAC) 2019-06-13
2016 Elena Toson, Marco Bevilacqua, Lorenzo Ferrario, Monica Valli, Pietro Guerrieri
D-Raise: A Propulsion System for GEO Satellite Platforms to Reduce Operational Risks and Time-to-Orbit
published pages: , ISSN: , DOI:
67th International Astronautical Congress (IAC) 2019-06-13
2016 Elena Toson, Alessio Fanfani, Simone Morosi, Luca Simone Ronga, Piermarco Martegani, Luca Rossettini
D-SAT MISSION: AN IN-ORBIT DEMONSTRATION OF A SOLID PROPELLANTSATELLITE DECOMMISSIONING DEVICE
published pages: , ISSN: , DOI:
Proceedings of the Small Satellites, System & Services Symposium (4S) 2019-06-13

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