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7th International Conference on Astrodynamics Tools and Techniques (ICATT)

6–9 Nov 2018
DLR Oberpfaffenhofen, Germany
Europe/Amsterdam timezone

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Session

On-orbit servicing and proximity #1

On-orbit servicing and proximity #1
8 Nov 2018, 09:00
DLR Oberpfaffenhofen, Germany

DLR Oberpfaffenhofen, Germany

Münchener Straße 20 82234 Weßling

Conveners

On-orbit servicing and proximity #1

  • Jean François GOESTER
  • Sarah Lammens (S&T)
  • Christina Jetzschmann (Airbus DS Bremen)

Description

Astrodynamics for re-fuelling, payload exchange, and tugging; rendezvous approach (far and close); computation of optimal phasing conditions; docking and mating; contact dynamics; berthing; docking in R-bar and V-bar; optimal ground contacts during rendezvous;

Presentation materials

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  1. 7. RICADOS - Rendezvous, Inspection, CApturing and Detumbling by Orbital Servicing
    Dr Heike Benninghoff (German Aerospace Center (DLR))
    08/11/2018, 09:00
    06: On-orbit servicing and proximity
    Oral presentation at the conference

    Safe de-orbiting and increasing the life-time of satellites by on-orbit servicing (OOS) will be of high importance in future spaceflight. The rendezvous and docking/berthing (RvD/B) phase is one of the most complex and critical parts of on-orbit servicing and debris removal missions. Several missions and developments have been started like the Restore-L mission of NASA, the RSGS (Robotic...

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  2. 22. Safe natural far Rendezvous approaches for Cislunar Near Rectilinear Halo Orbits in the Ephemeris model
    Mr Emmanuel Blazquez (ISAE-Supaéro)
    08/11/2018, 09:30
    06: On-orbit servicing and proximity
    Oral presentation at the conference

    In the context of future Human Spaceflight exploration missions, Rendezvous and Docking (RVD) operational activities are mandatory and critical for the assembly and maintenance of cislunar structures [1]. The Orion spacecraft is expected to handle cargo delivery and crew exchange missions that will all require RVD. Despite extensive experience in Low Earth and Low Lunar Orbits, no operational...

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  3. 25. ROSSONERO: a tool for preliminary rendezvous mission design in the restricted three-body problem
    Giordana Bucchioni (University of Pisa, Department of Information Engineering)
    08/11/2018, 10:00
    06: On-orbit servicing and proximity
    Oral presentation at the conference

    Extended abstract

    The present international cooperation scenario for robotic and human space exploration is focusing on mission architectures that revolve around building and exploiting a crew-tended cis-lunar space station, known as Lunar Orbital Platform-Gateway. Candidate orbits for this vehicle are the near rectilinear halo orbits (NRHO). Therefore, the capability to inject in NRHO...

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