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  • Modelling the Stability of Different Re-entry Capsule Shapes
    Modelling reentry capsule shape In addition, it is believed that the synergistic use of experimental, theoretical and numerical techniques used by the team represents a valuable example of how to properly tackle a complex multi-physical problem as the atmospheric entry More about this activity is available in the TDE Highlights brochure 2022
  • Trajectory Planning and Tracking for a Re-Entry Capsule with a . . . - MDPI
    In the last decade, the increasing use of NanoSats and CubeSats has made the re-entry capsule an emerging research field needing updates in configuration and technology In particular, the door to advancements in terms of efficiency and re-usability has been opened by the introduction of inflatable and or deployable aerodynamic brakes and the use of on-board electronics for active control
  • Design and material optimization of an Orion re-entry aeroshell for . . .
    Space exploration and interplanetary missions are achieved using re-entry capsules for both manned and unmanned missions Re-entry capsules experience a higher amount of pressure and temperatures during re-entry which induces aerodynamic heating further leading to structural deformation due to shear stress [1]
  • The heat shield of Artemis 2 aced a wonderful test
    Validating the performance of the heat shield of Artemis 2 is essential for refining thermal protection systems for future deep space travel Theories regarding charring behavior led engineers to optimize the reentry path, ensuring the Orion capsule could withstand planetary return speeds without catastrophic structural failure
  • AERODYNAMIC STABILITY ANALYSIS AND DESIGN OF A RE-ENTRY CAPSULE FOR A . . .
    The focus of this study is mainly on the aero-shell design of the capsule, in order to achieve the stability required for a successful re-entry
  • Successful reentries and extreme temperatures: The year in . . .
    This groundbreaking research utilized Varda Space Industries’ W-2 hypersonic capsule to collect in situ shock layer radiative emission measurements during its reentry into Earth’s atmosphere at conditions ranging from Mach 29 5–15 0 and altitudes of 105-50 kilometers, respectively
  • EURASTROS capsule design and re-entry analysis - EUCASS
    In this study, the capsule of the EURASTROS study is discussed in terms of its aerodynamic and aero-thermal properties, re-entry characteristics, structural design, and thermal protection system
  • Reentry Capsule Reachable Tube Boundary Prediction via Evolutionary . . .
    To enhance prediction efficiency, ensure data accuracy, reduce calculation time, and ultimately improve the performance of the planning system, this paper proposes a novel method for predicting the reachable tube boundary of a parachute recovery system
  • Reentry capsule - Wikipedia
    The capsule design is both volumetrically efficient and structurally strong, so it is typically possible to construct small capsules of performance comparable to lifting body or spaceplane designs in all but lift-to-drag ratio for less cost
  • Design and efficiency assessment of hybrid thermal protection . . .
    Here, we report on different types of hybrid TPSs to improve the heat-shielding performance An ablative-thermal-structural analysis model was first established based on the finite element method, and optimization analyses were performed to determine the sizes of the hybrid structures





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