indico will be upgraded to the latest version on Tuesday 10th Decmeber. It may be unavailable all day.

Login

Clean Space Industrial Days & AeroThermoDynamics Design for Demise Workshop

24–26 Oct 2017
ESTEC
UTC timezone

Contribution List

119 / 119
144. Opening Speech
24/10/2017, 09:00
145. Market for ADR
Alberto Accogli (Leoni Coporate Advisors)
24/10/2017, 09:20
146. Critical raw materials and their role in the European aerospace and energy sectors
Evangelos Tzimas (European Commision - DG Joint Research Centre)
24/10/2017, 09:45
147. Space Debris Mitigation implementation in Earth Observation Missions
Guido Levrini (ESA)
24/10/2017, 10:10
148. Clean Space overview
Luisa Innocenti (ESA)
24/10/2017, 10:35
52. e.Deorbit & SSV
Mr Robin Biesbroek (ESA)
24/10/2017, 11:30
65. EcoDesign at ESA
Ms Sara Morales Serrano (ESA)
24/10/2017, 11:30
39. Large System Integrator SDM technology priorities
Daniel Briot (ADS), Mr Gerrit Proffe (OHB System AG), Lilith Grassi (TAS)
24/10/2017, 11:30
66. LCA of launchers environmental impact
Augustin Chanoine (Deloitte)
24/10/2017, 11:50
53. Results of the Airbus DS led e.Deorbit Phase B1 ESA study
Dr Stéphane Estable (Airbus)
24/10/2017, 11:50
67. LCA of satellites environmental impact
Augustin Chanoine (Deloitte)
24/10/2017, 12:10
56. Space Debris Attitude Motion Measurements and Modelling, ENVISAT Case
Jiri Silha (University of Bern)
24/10/2017, 12:10
40. Technology priorities for small satellites
Peter Holsters (QinetiQ)
24/10/2017, 12:10
41. Ariane 6 approach and solutions regarding space debris mitigation
Nathalie Dias (Ariane Group)
24/10/2017, 12:30
59. Final Pre-Flight Update for the Remove Debris ADR Mission
Jason Forshaw
24/10/2017, 12:30
150. Question & Answers
24/10/2017, 12:30
68. EcoDesign: Towards Life Cycle Sustainability of Space Systems
Mr Andrew Wilson (University of Strathclyde)
24/10/2017, 14:00
54. Space Transportation Bus: An opporunity for new possibilities of Space Exploitation or Space Tug
Mrs carole billot (thales alenia space france)
24/10/2017, 14:00
46. State of the art overview
François Bausier (ESA)
24/10/2017, 14:00
47. Battery safety assessment and testing
Bruno Samaniego Lopez (Airbus Defence and Space)
24/10/2017, 14:20
69. Space OPERA: integrating environmental performance into concurrent design
Augustin Chanoine
24/10/2017, 14:20
57. Space Tug
Mr Gerrit Proffe (OHB System AG), Marc Scheper (OHB)
24/10/2017, 14:20
70. Lessons learned from the Sentinel 3 LCA and Applications to a GreenSat
Mr Nicolas Thiry (Thales Alenia Space)
24/10/2017, 14:40
48. Solar Array Passivation based on the galvanic isolation
Vincent Lempereur (TAS)
24/10/2017, 14:40
55. Space Utility vehichle
Eugenio Ferreira (Airbus)
24/10/2017, 14:40
49. Assessment of risk of debris generation due to battery failure in cubesats
Alessandro Chiesa (Aviospace)
24/10/2017, 15:00
71. Ecodesign applied to ESA’s PROBA-Vegetation satellite
An vercalsteren (Vito NV)
24/10/2017, 15:00
58. Utilising the Space Drone spacecraft for ADR
Ms Danna Linn Barnett (Effective Space Solution)
24/10/2017, 15:00
60. ESA GNC Technologies and Test Beds for ADR and Space Tug Applications
Dr Guillermo Ortega (ESA)
24/10/2017, 16:00
72. Impacts of space vehicles' launch and re-entry on the ozone layer and climate
Slimane Bekki (CNRS)
24/10/2017, 16:00
42. System impacts of propulsion passivation
Andreas Gernoth (ESA)
24/10/2017, 16:00
73. Atmospheric impact of spacecraft demise
Lilith Grassi (Thalès Alenia Space)
24/10/2017, 16:20
61. On-ground testing of vision-based navigation for non-cooperative rendezvous targets using cameras in the visible and thermal infrared range
Manuel Sanchez Gestido (ESA)
24/10/2017, 16:20
43. SMA Valve for fluidic passivation
Mr Stephan Kraus (ariane group)
24/10/2017, 16:20
74. Experimental Modelling of Alumina Particulate in Solid Booster
Dominik Saile (DLR)
24/10/2017, 16:40
62. Investigation of Detumbling Techniques
Fernando Gandia (GMV)
24/10/2017, 16:40
44. Life time extension of pyro actuations for passivation
Pierre Joanny (Dassault Aviation)
24/10/2017, 16:40
63. COMRADE
Fernando Gandía Abellán (GMV)
24/10/2017, 17:00
75. Impact on atmosphere and ocean
Sophia Klink (Université de Montpellier)
24/10/2017, 17:00
45. Passivation device for Spacecraft Propulsion System
Mr DENIS DILHAN (CNES)
24/10/2017, 17:00
64. HIPNOS: High Performance Avionics Solution for Advanced and Complex GNC Systems for ADR
Mr David Gonzalez-Arjona (GMV Aerospace and Defence)
24/10/2017, 17:20
76. Questions & Answers
24/10/2017, 17:20
50. Sentinel-1 Space Debris Mitigation
Svein Lokas (ESA)
24/10/2017, 17:20
51. Space Tugs economics Round Table
24/10/2017, 18:00
This discussion will cover a number of key issues to this emerging niche market such as the challenges, competition, cost uncertainties, tug use case analysis.
113. LCA space propellants Round Table
25/10/2017, 09:30
This session will begin by presenting an ESA study which performed the Life Cycle Assessment of space propellants. The methodology and results will be presented followed by open discussion afterwards regarding implications for green propellants, major considerations for reducing environmental impact, and scale up from lab to industrial scale.
78. Overview of CNES SRL activities related to the compliance of the satellites with French Space Act
Pierre Omaly (CNES)
25/10/2017, 09:30
96. Technology building blocks and ongoing activities regarding spectral sensing for relative navigation
Dr Marco Esposito (cosine Research BV)
25/10/2017, 09:30
77. Characterisation of the behaviour of typical spacecraft materials exposed to re-entry environment conditions
Benoit Bonvoisin (ESA)
25/10/2017, 09:50
97. The RVS3000 and the RVS 3000-3D LIDAR Sensors: Recent Technological Advances and Future Applications
Florian Kolb (Jena Optronik)
25/10/2017, 09:50
79. Demisable materials database
Dr James Merrifield (Fluid Gravity Engineering)
25/10/2017, 10:10
98. ORCO: End-to-end On Ground System Validation of combined technologies for Debris Removal
Fernando Gandía Abellán (GMV)
25/10/2017, 10:10
80. The Horizon 2020 ReDSHIFT Project: 3D printing of demisable spacecraft
Dr Alessandro Rossi (IFAC-CNR)
25/10/2017, 10:30
99. VIMANCO: Vision Manipulation of non-cooperative objects
Vassilios Papantoniou (HTR)
25/10/2017, 10:30
81. Reentry tools: DRAMA upgrade and reentry tumbling state with IOTA
Ronny Kanzler (HTG)
25/10/2017, 10:50
100. Using Infrared-base relative navigation for Active Debris Removal
Özgün Yilmaz (University Cranfield, UK / ESA)
25/10/2017, 10:50
82. Demise Observation Capsule: Progress update
Trevor Watts (Science & Technology B.V)
25/10/2017, 11:10
101. Navigation on a chip
Florian Kolb (Jena Optronik)
25/10/2017, 11:10
102. ESA Robotics for ADR and Space Tug Applications
Gianfranco Visentin (ESA)
25/10/2017, 11:50
83. Multidisciplinary assessment of D4D techniques
Ronny Kanzler (HTG)
25/10/2017, 11:50
114. Single Score Round Table
25/10/2017, 11:50
Within Life Cycle Assessment, certain environmental indicators may be of more interest than others. This session aims to make a prioritisation to define the most important environmental indicators and to discuss weighting factors between them in order to arrive at a 'single score for space' agreed upon by space sector actors.
84. D4OP – Demisability for Optical Payloads
Simone Bianchi (TAS)
25/10/2017, 12:10
103. Development of a gripper and the associated MGSE equipment
Mr Jaroslaw Jaworski (PIAP Space)
25/10/2017, 12:10
85. Demisability of Optical Payloads
Dr James Beck (Belstead Research Ltd)
25/10/2017, 12:30
104. PREDATOR : ENVISAT capturing strategy using a STEWART platform based gripper
Stelios Skevakis (HTR)
25/10/2017, 12:30
86. Identification of re-entry critical launch vehicle components
Mr Stijn Lemmens (European Space Agency)
25/10/2017, 12:50
105. Using a plenoptic camera for vision based navigation in an Active Debris Removal scenario
Jonas Philipp Lüke (Universidad de La Laguna)
25/10/2017, 12:50
115. Can citric acid be used as an environmentally friendly alternative to nitric acid passivation for steel? An experimental and Life Cycle Assessment (LCA) study
Christopher Zimdars (Quantis), Usoa Izagirre (TECNALIA)
25/10/2017, 14:00
87. Design and breadboarding of technologies for early breakup of spacecraft
Mr Gerrit Proffe (OHB System AG)
25/10/2017, 14:00
106. Pre-Development of a Clamping Mechanism
Mr Iñigo Sard (AVS)
25/10/2017, 14:00
116. Alternative pretreatments to aluminium
Ana G. Pereira (ISQ)
25/10/2017, 14:20
88. Demisable joint
Lilith Grassi (TAS)
25/10/2017, 14:20
107. Design and Performance Analysis of the DLR robot manipulator arm for the e.Deorbit mission
Roberto Lampariello (DLR)
25/10/2017, 14:20
89. Demisable joints CleanSat study
Mr Stephan Kraus (ariane group)
25/10/2017, 14:40
117. REACH replacement of pyrovalve initiator powder
Pierre Joanny (Dassault Aviation)
25/10/2017, 14:40
108. Validation Methodology of the Rendezvous and Grasping Maneuver on the Planar Air-Bearing Microgravity Simulator
Dr Karol Seweryn (Space Research Centre PAS (CBK PAN))
25/10/2017, 14:40
109. ASSIST
Dario Mora
25/10/2017, 15:00
118. How to assess REACH-related obsolescence risk in early design?
Augustin Chanoine (Deloitte), Tim Becker (ReachLaw)
25/10/2017, 15:00
90. Questions & Answers
25/10/2017, 15:00
119. Natural fiber composites for space applications
Mr Julien Rion (Bcomp SA)
25/10/2017, 15:10
91. Containment tether
Mr Gerrit Proffe (OHB System AG)
25/10/2017, 16:00
120. Space Sustainability in the 21st Century
Jorge Del Rio Vera (UNOOSA)
25/10/2017, 16:00
The presentation will explain the different initiatives in which the United Nations Office for Outer Space Affairs is involved regarding sustainability of outer space and how these initiatives are related to UNISPACE+50, the special segment of the United Nations Committee on the Peaceful Uses of Outer Space and the Space 2030 agenda.
35. Tethered-tugs dynamics and control verification and models validation by 0g experiments on parabolic flights
Prof. Michelle Lavagna (Politecnico di Milano)
25/10/2017, 16:00
The paper presents in details the design, implementation and running of the experiment run by the PoliTethers DAERPoliMi team to verify and validate the flexible connections dynamics in the 0g relevant environment. Space Tugs exploiting tether connection with the target must avoid effects such the bounce back and whiplash provoked by the intrinsic tether flexibility and elasticity. Therefore,...
92. Demisability Assessment of Reaction Wheels
Geert Smet (ESA)
25/10/2017, 16:20
36. Design and Dynamic Testing of Tether System as Active Capture Technology for e.Deorbit and Net/Harpoon Based Missions
Dr Lorenzo Marconi (Arescosmo S.p.A.)
25/10/2017, 16:20
The concept of space tethers has great potential in space applications; for this reason they have been investigated as electrodynamics power generators or motors, momentum exchange and orbital stabilization assets or formation flying connection and pulling ropes. In the most recent years, in the context of ESA (European Space Agency) Clean Space Initiative and general interest in space debris...
121. Spacecraft design indicator fo space debris
Dr Camilla Colombo (Politecnico di Milano)
25/10/2017, 16:20
93. Demisable materials compatibility for Tanks
Adam Watts (Nammo Westcott Ltd)
25/10/2017, 16:40
110. ISS SPHERES Tether Dynamics Experiments / Evaluation of Tethered Active Debris Removal Issues
Mr Marcel Becker (German)
25/10/2017, 16:40
122. Towards the consideration of space debris within the Life Cycle Assessment Framework
Mr Thibaut Maury (Ariane Group / Univ. Bordeaux)
25/10/2017, 16:40
94. Demisable propellant tank design
Renato Bellarosa (Airbus), Sylvain Goek (Ariane Group)
25/10/2017, 17:00
111. Full Scale Demonstration of Debris Capturing with Deployable Nets
Wojtciech Golebiowski (SKA Polska)
25/10/2017, 17:00
123. Simulating the Beginning of the Congestion-Tipping Period for Earth Orbits
Michel van Pelt (ESA)
25/10/2017, 17:00
Earth Orbits are a finite resource. Understandably, this statement is difficult to fathom given the vastness of space, yet Earth orbits are not infinite regions in this vastness. This study proves that Earth orbits are a limited, natural resource and goes on to construct a quantitatve model to estimate the beginning of the period beyond which it would be detrimental for satellites to continue...
124. Economic value of space debris
Romain Esteve (Toulouse School of Economics (TSE))
25/10/2017, 17:20
112. PATENDER: A Net-Based Experiment and Possible Solution to the Space Debris Problem
Lorenzo Cercos (GMV)
25/10/2017, 17:20
95. Questions & Answers
25/10/2017, 17:20
125. Sustainability of Space Round Table
25/10/2017, 18:00
The session aims to discuss how we can define and quantify the sustainability of space, both from an Earth and orbital perspective.
38. Semi-controlled re-entry Round Table
26/10/2017, 09:00
Semi-controlled reentry can reduce the impact of controlled reentry at system level, but domains of feasibility and uncertainties must be quantified as well as the respective legal implications.
137. e.Inspector - a cubesat inspection mission
Ms Sara Morales Serrano (ESA)
26/10/2017, 11:30
127. Environmental impact of passive deorbit devices
Dr Camilla Colombo (Politecnico di Milano)
26/10/2017, 11:30
138. Inspection trajectories and GNC design
Mr Eric Reinthal (University of Würzburg), Dr Jesus Gil (ESA/ESTEC)
26/10/2017, 11:40
128. ADEO Passive De-Orbit Subsystem Activity leading to a Dragsail Demonstrator: Conclusion and Next Steps
Mrs Thomas Sinn (HPS GmbH)
26/10/2017, 11:50
139. High thrust chemical propulsion for small satellites
Tobias Knop (Hyperion Technologies)
26/10/2017, 12:00
129. Electrostatic tether plasma brake module for deorbiting
Dr Pekka Janhunen (Finnish Meteorological Institute)
26/10/2017, 12:10
140. Efficient De-Orbiting of Micro and Nano Satellites Using the IFM Nano-Thruster
Mr Alexander Reissner (FOTEC)
26/10/2017, 12:20
130. Customer-driven deorbit kit based on bare electrodynamic tether technology
Mr Eduardo Urgoiti (SENER)
26/10/2017, 12:30
152. Nanosat propulsion systems
Zeger de Groot (ISIS)
26/10/2017, 12:40
141. Mega Constellations EOL operations
Kate Symonds (ESA)
26/10/2017, 14:00
131. Overview of technologies for controlled deorbit
Mr Tiago Soares (ESA)
26/10/2017, 14:00
142. Active Debris Removal: A possible solution for megaconstellations
Mrs carole billot (thales alenia space france)
26/10/2017, 14:20
132. Electronic pressurant regulator
Adam Watts (Nammo Westcott Ltd)
26/10/2017, 14:20
133. Arcjet
Stefan Gregucci (Sitael)
26/10/2017, 14:40
143. Design for Removal: A cost efficient opportunity to prepare future satellites to an an ADR mission
Mrs carole billot (thales alenia space france)
26/10/2017, 14:40
134. Deorbit Motors for Active Deorbiting
Ulrich Gotzig (Ariane Group)
26/10/2017, 15:30
149. Reliability Round Table
26/10/2017, 15:30
The requirement on reliability is evolving from a conditional success probability of the End of Life operations to an absolute value. The consequences at system and subsystem level will be discussed as well as the approach to determine the reliability at end of life and evaluate mission extensions.
135. Conceptual design of Solid Rocket Motor for deorbitation and advances in the development of an Aluminium-free solid propellant
Adam Okniński (Institute of Aviation)
26/10/2017, 15:50
136. D-SAT Mission: an In-Orbit Demonstration of Satellite Controlled Re-entry
Alessio Fanfani (D-Orbit)
26/10/2017, 16:10
151. Assessment of risk of debris generation due to battery failure in cubesats: the cuba project
5. DESIGN AND DYNAMIC TESTING OF TETHER SYSTEM AS ACTIVE CAPTURE TECHNOLOGY FOR E.DEORBIT AND NET/HARPOON-BASED MISSIONS
Dr Andrea Messidoro (Arescosmo S.p.A.), Dr Lorenzo Marconi (Arescosmo S.p.A.)
The concept of space tethers has great potential in space applications; for this reason they have been investigated as electrodynamics power generators or motors, momentum exchange and orbital stabilization assets or formation flying connection and pulling ropes. In the most recent years, in the context of ESA (European Space Agency) Clean Space Initiative and general interest in space debris...
126. Semi-controlled reentry can reduce the impact of controlled reentry at system level, but domains of feasibility and uncertainties must be quantified as well as the respective legal implications.
37. The requirement on reliability is evolving from a conditional success probability of the End of Life operations to an absolute value. The consequences at system and subsystem level will be discussed as well as the approach to determine the reliability at end of life and evaluate mission extensions.
Powered by Indico v3.3.5