Login

Clean Space Industrial Days & AeroThermoDynamics Design for Demise Workshop

24–26 Oct 2017
ESTEC
UTC timezone

Session

CleanSat

24 Oct 2017, 11:30
Erasmus building (ESTEC)

Erasmus building

ESTEC

ESTEC Keplerlaan 1 Noordwijk

Presentation materials

There are no materials yet.

  1. 39. Large System Integrator SDM technology priorities
    Daniel Briot (ADS), Mr Gerrit Proffe (OHB System AG), Lilith Grassi (TAS)
    24/10/2017, 11:30
  2. 40. Technology priorities for small satellites
    Peter Holsters (QinetiQ)
    24/10/2017, 12:10
  3. 41. Ariane 6 approach and solutions regarding space debris mitigation
    Nathalie Dias (Ariane Group)
    24/10/2017, 12:30
  4. 46. State of the art overview
    François Bausier (ESA)
    24/10/2017, 14:00
  5. 47. Battery safety assessment and testing
    Bruno Samaniego Lopez (Airbus Defence and Space)
    24/10/2017, 14:20
  6. 48. Solar Array Passivation based on the galvanic isolation
    Vincent Lempereur (TAS)
    24/10/2017, 14:40
  7. 49. Assessment of risk of debris generation due to battery failure in cubesats
    Alessandro Chiesa (Aviospace)
    24/10/2017, 15:00
  8. 42. System impacts of propulsion passivation
    Andreas Gernoth (ESA)
    24/10/2017, 16:00
  9. 43. SMA Valve for fluidic passivation
    Mr Stephan Kraus (ariane group)
    24/10/2017, 16:20
  10. 44. Life time extension of pyro actuations for passivation
    Pierre Joanny (Dassault Aviation)
    24/10/2017, 16:40
  11. 45. Passivation device for Spacecraft Propulsion System
    Mr DENIS DILHAN (CNES)
    24/10/2017, 17:00
  12. 50. Sentinel-1 Space Debris Mitigation
    Svein Lokas (ESA)
    24/10/2017, 17:20
  13. 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
  14. 77. Characterisation of the behaviour of typical spacecraft materials exposed to re-entry environment conditions
    Benoit Bonvoisin (ESA)
    25/10/2017, 09:50
  15. 79. Demisable materials database
    Dr James Merrifield (Fluid Gravity Engineering)
    25/10/2017, 10:10
  16. 80. The Horizon 2020 ReDSHIFT Project: 3D printing of demisable spacecraft
    Dr Alessandro Rossi (IFAC-CNR)
    25/10/2017, 10:30
  17. 81. Reentry tools: DRAMA upgrade and reentry tumbling state with IOTA
    Ronny Kanzler (HTG)
    25/10/2017, 10:50
  18. 82. Demise Observation Capsule: Progress update
    Trevor Watts (Science & Technology B.V)
    25/10/2017, 11:10
  19. 83. Multidisciplinary assessment of D4D techniques
    Ronny Kanzler (HTG)
    25/10/2017, 11:50
  20. 84. D4OP – Demisability for Optical Payloads
    Simone Bianchi (TAS)
    25/10/2017, 12:10
  21. 85. Demisability of Optical Payloads
    Dr James Beck (Belstead Research Ltd)
    25/10/2017, 12:30
  22. 86. Identification of re-entry critical launch vehicle components
    Mr Stijn Lemmens (European Space Agency)
    25/10/2017, 12:50
  23. 87. Design and breadboarding of technologies for early breakup of spacecraft
    Mr Gerrit Proffe (OHB System AG)
    25/10/2017, 14:00
  24. 88. Demisable joint
    Lilith Grassi (TAS)
    25/10/2017, 14:20
  25. 89. Demisable joints CleanSat study
    Mr Stephan Kraus (ariane group)
    25/10/2017, 14:40
  26. 90. Questions & Answers
    25/10/2017, 15:00
  27. 91. Containment tether
    Mr Gerrit Proffe (OHB System AG)
    25/10/2017, 16:00
  28. 92. Demisability Assessment of Reaction Wheels
    Geert Smet (ESA)
    25/10/2017, 16:20
  29. 93. Demisable materials compatibility for Tanks
    Adam Watts (Nammo Westcott Ltd)
    25/10/2017, 16:40
  30. 94. Demisable propellant tank design
    Renato Bellarosa (Airbus), Sylvain Goek (Ariane Group)
    25/10/2017, 17:00
  31. 95. Questions & Answers
    25/10/2017, 17:20
  32. 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.
    Go to contribution page
  33. 127. Environmental impact of passive deorbit devices
    Dr Camilla Colombo (Politecnico di Milano)
    26/10/2017, 11:30
  34. 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
  35. 129. Electrostatic tether plasma brake module for deorbiting
    Dr Pekka Janhunen (Finnish Meteorological Institute)
    26/10/2017, 12:10
  36. 130. Customer-driven deorbit kit based on bare electrodynamic tether technology
    Mr Eduardo Urgoiti (SENER)
    26/10/2017, 12:30
  37. 131. Overview of technologies for controlled deorbit
    Mr Tiago Soares (ESA)
    26/10/2017, 14:00
  38. 132. Electronic pressurant regulator
    Adam Watts (Nammo Westcott Ltd)
    26/10/2017, 14:20
  39. 133. Arcjet
    Stefan Gregucci (Sitael)
    26/10/2017, 14:40
  40. 134. Deorbit Motors for Active Deorbiting
    Ulrich Gotzig (Ariane Group)
    26/10/2017, 15:30
  41. 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
  42. 136. D-SAT Mission: an In-Orbit Demonstration of Satellite Controlled Re-entry
    Alessio Fanfani (D-Orbit)
    26/10/2017, 16:10
Building timetable...