Skip to main content

Multi-Functional Interface for Flexibility and Reconfigurability of Future European Space Robotic Systems


The capabilities of maximising standard payload modules’ functionalities for applications such as on-orbit satellite servicing or planetary exploration depend critically on the creation and availability of a standard interface (IF). Standard interface should provide, aside from the necessary mechanical interconnections, electrical power and data connections, as well as thermal transfer between “building block” payload modules. The overall flexibility enabled by such IF will allow endless reconfigurations of payload and other modules for different functional requirements. This can be considered a game changer technology, enabling transformation from the current approach to space missions, deploying single-use system with pre-planned and limited functionalities, to a radically new approach with multi-use, dynamically reconfigurable and multi-functional systems. Hence, SIROM aims to set a new research agenda for future affordable space missions. Within this context, the partners of the SIROM (Standard Interface for Robotic Manipulation of payloads in future space missions) project are developing the first standard IF solution that combines the four required functionalities in an integrated and compact form for future space missions. With a mass lower than 1.5 kg and having an external diameter of 120 mm and a height of 30 mm, this novel interface permits not only mechanical coupling but also electrical, data and thermal connectivity between so called Active Payload Modules (APMs), as well as other modules such as the robotic end-effectors. This multi-functional IF features an androgynous design to allow for replacement and reconfiguration of the individual modules in any combination desired. It consists of the following sub-assemblies: mechanical IF, electrical IF, data IF, thermal IF and IF controller. A clear advantage of SIROM design is that its mechanical IF consists of a latching and guiding systems for misalignment correction, capable of withstanding certain robotic arm positioning inaccuracies: ± 5 mm translation and ± 1.5° rotation in all axes. Regarding the electrical and data IFs, SIROM transfers up to 150 W electrical power and provides a data transfer rate of 100 Mbit/s via SpaceWire, plus command communication with speeds up to 1Mbit/s via CAN bus. The thermal IF provides fluidic ports for flow transfer and has the potential to transfer 2500 W between APMs accordingly provided with the corresponding close-loop heat exchange system. Although not envisaged for SIROM current design, a possible variation could be to use these ports for satellite re-fuelling. Apart from that, SIROM exhibits redundant coupling capabilities: it can match and couple another completely passive SIROM. It is provided with main and redundant connectors for thermal, electrical, data and control flow in case of one of the lines fails. All in all, SIROM will enable long duration missions with no logistic support, refurbishing, maintenance and reconfiguration of satellites, cost efficiency and simplification of the tool exchange in scientific exploration missions. SIROM is designed to be a common building block for European and possibly world future space robotics enabled missions.

This is a preview of subscription content, access via your institution.

Fig. 1

(credit NASA/Goddard Space Flight Center 2017)

Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13

(credit DFKI GmbH 2018)

Fig. 14

(credit DFKI GmbH 2018)

Fig. 15

(credit DFKI GmbH)

Fig. 16

(credit DFKI GmbH)

Fig. 17

(credit DFKI GmbH)

Fig. 18
Fig. 19
Fig. 20



Active payload module




Standard interface for robotic manipulation of payloads in future space missions


Electrical ground support equipment


On-orbit servicing


Low Earth orbit


Multi-robot system


On board computer


  1. 1.

    Vinals J, Urgoiti E, Guerra G, Valiente I, Esnoz J, Ilzkovitz M, Cetin D, Letier P, Yan X, Henry G, Quaranta A, Brinkmann W, Jankovic M, Bartsch S, Kollias V, Pogkas N, Fumagalli A, Doermer M (2018) Future space missions with reconfigurable modular payload modules and standard interface—an overview of the SIROM project, IAC-18-d3.2. In: 69th International Astronautical Congress, Bremen, Germany, 1–5 October 2018

  2. 2.

    Standard interface for robotic manipulation of payloads in future space missions, project summary. Accessed 12 June 18

  3. 3.

    Yan X-T, Brinkmann W, Palazzetti R, Melville C, Li Y, Bartsch S, Kirchner F (2018) Integrated mechanical, thermal, data, and power transfer interfaces for future space robotics. Front Robot AI 5:64.

    Article  Google Scholar 

  4. 4.

    Palazzetti R, Donaldson K, Wenzel W, Bartsch S, Yan X-T (2017) Toward a multifunctional interface for future planetary and orbital missions, IAC-18-D3.2. In: 68th Int. Astronautical Congress, Adelaide, Australia

  5. 5.

    Kortman M, Ruhl S, Weise J, Kreisel J, Schervan T, Schmidt H, Dafnis A (2015) Building block based iBoss approach: fully modular systems with standard interface to enhance future satellites. In: 66th International Astronautical Congress. Israel, Jerusalem, pp 1–11

  6. 6.

    Jankovic M, Brinkmann W, Bartsch S, Palazzetti R, Yan X (2018) Concepts of active payload modules and end-effectors suitable for Standard Interface for Robotic Manipulation of Payloads in Future Space Missions (SIROM) interface. In: Proceedings of the 2018 IEEE Aerospace Conference, IEEE Aerospace Conference, 2018, Big Sky, Montana, USA, pp 1–16

  7. 7.

    Alario JP and Otterstedt PJ (1985) A heat pipe quick disconnect. In: 15th Intersociety Conference on Environmental Systems, California, 1985

  8. 8.

    Lefèvre J, Charles S, Bosch M, Eynard B, Henner M (2010) Multidisciplinary Simulation of Mechatronic Components in Severe Environments. In: Aiguier M, Bretaudeau F, Krob D (eds) Complex Syst. Des. Manag. Proc. First Int. Conf. Complex Syst. Des. Manag. CSDM 2010. Springer, Berlin, pp 295–304.

    Chapter  Google Scholar 

  9. 9.

    Hehenberger P (2014) Perspectives on hierarchical modeling in mechatronic design. Adv Eng Inform 28:188–197.

    Article  Google Scholar 

  10. 10.

    Zheng C, Hehenberger P, Le Duigou J, Bricogne M, Eynard B (2016) Multidisciplinary design methodology for mechatronic systems based on interface model. Res Eng Des.

    Article  Google Scholar 

  11. 11.

    Corke P (2011) Vision-based control. In: Robotics, vision and control. Springer tracts in advanced robotics, vol 73. Springer, Berlin, pp 455–479

    Google Scholar 

  12. 12.

    Cordes F, Babu A, Sherpa TT (2016) A versatile hybrid wheeled-leg rover. In: Proceedings of the 13th International Symposium on Artificial Intelligence, Robotics and Automation in Space, (iSAIRAS-16), Beijing, 20th–23rd June 2016

Download references


The authors would like to thank all the supporting staff and partners of the SIROM Project: SENER (Spain), Airbus DS Ltd. (UK), Airbus DS GmbH (Germany), Thales Alenia Space S.p.A (Italy), Leonardo S.p.A. (Italy), the University of Strahclyde (UK), German Research Center for Artificial Intelligence (DFKI), Robotics Innovation Center(Germany), TELETEL (Greece), Space Applications Services N.V. (Belgium) and MAG SOAR S.L. (Spain). SIROM is part of the PERASPERA project on Space Robotics Technologies, and has received funding from the European Union’s Horizon 2020 research and innovation programme under Grant agreement no 730035.

Author information



Corresponding authors

Correspondence to Javier Vinals or Xiu-Tian Yan.

Rights and permissions

Reprints and Permissions

About this article

Verify currency and authenticity via CrossMark

Cite this article

Vinals, J., Urgoiti, E., Guerra, G. et al. Multi-Functional Interface for Flexibility and Reconfigurability of Future European Space Robotic Systems. Adv. Astronaut. Sci. Technol. 1, 119–133 (2018).

Download citation


  • Space robotic
  • Space interface
  • Orbital missions
  • Orbital payload
  • Standard interface
  • Multifunctional interface