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European Space Thermal Engineering Workshop 2019

8–10 Oct 2019
ESA/ESTEC
Europe/Amsterdam timezone

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Session

Small Satellites and CubeSats / Analysis

CS
9 Oct 2019, 14:00
Newton 1

Newton 1

Conveners

Small Satellites and CubeSats / Analysis

  • Philipp Hager (ESA)

Presentation materials

There are no materials yet.

  1. 7. A Modular Approach to Thermal Modelling of CubeSats in ESATAN-TMS
    Mr Arne te Nijenhuis (NLR - Royal Netherlands Aerospace Centre)
    09/10/2019, 14:00
    thermal technologies and methodologies related to small satellites and CubeSats

    With the CubeSat market expanding and with CubeSats entering the high-performance domain (to 6U, 12U and 16U) the thermal problems of CubeSats get more prominent. A result of the shift towards high-performance missions leads to stricter thermal requirements as the power density increases and the usual low cost thermal design strategies appear insufficient.

    An innovative modular thermal...

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  2. 8. Modular Parallel Micro Pump for Adaptive Thermal Control of CubeSats
    Ramon van den Berg (NLR)
    09/10/2019, 14:30
    thermal technologies and methodologies related to small satellites and CubeSats

    With the CubeSat market expanding and with CubeSats entering the high-performance domain (to 6U, 12U and 16U) the thermal problems of CubeSats get more prominent. A result of the shift towards high-performance missions leads to stricter thermal requirements as the power density increases and the usual low cost thermal design strategies appear insufficient.
    To further support the higher power...

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  3. 55. Radiative Surface Properties of a Trihedral Array for Lunar Thermal Control Applications
    Dr Colin Butler (University of Limerick)
    09/10/2019, 15:00
    thermal technologies and methodologies related to small satellites and CubeSats

    The increasing trend towards higher power electronics and the rapid growth of the smallsat industry has led to increased heat dissipation requirements for spacecraft thermal control systems. In this study, an investigation of a trihedral geometry is performed in order to determine its potential as an effective radiator panel for passive thermal management. This form aims to minimise the...

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  4. 6. The Application of a Thermal Mathematical Model during Lander Operations on the surfaces of Small Bodies
    Mr Michael Maibaum (German Aerospace Center)
    09/10/2019, 15:30
    thermal analysis and software tools

    Landing on small bodies like asteroids and comets is an extreme challenging operation. The unknown thermal and physical properties of the surface after a multi-annual journey in deep space require a high degree of flexibility for operations planning and execution during the landing and consecutive on-surface mission phases.
    The presentation describes the planning and analysis loop used to...

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