Ara es mostren els items 1-11 de 11

    • A simulation tool for parachute/payload systems 

      Flores Le Roux, Roberto Maurice; Ortega, Enrique; Vallés Fluvià, J.; Oñate Ibáñez de Navarra, Eugenio (Centre Internacional de Mètodes Numèrics en Enginyeria (CIMNE), 2014)
      Text en actes de congrés
      Accés restringit per política de l'editorial
      The design and evaluation of parachute-payload systems is a technology field in which numerical analysis tools can make very important contributions. This work describes a new development from CIMNE in this area, a coupled ...
    • Aeroelastic analysis of parachute deceleration systems with empirical aerodynamics 

      Ortega, Enrique; Flores Le Roux, Roberto Maurice (2019-11-13)
      Article
      Accés obert
      A technique for the aeroelastic solution of parachute decelerators is presented in this work. The methodology uses empirical aerodynamics, based on a filling-time inflation model and Ludtke's area law, coupled to two ...
    • Caracterización de una campana deportiva ram-air 

      Badia Alarcón, Arnau (Universitat Politècnica de Catalunya, 2021-10-28)
      Treball Final de Grau
      Accés restringit per decisió de l'autor
      Realitzat a/amb:   CIMSA
      Unlike the wing of an airplane, nowadays, there are not advanced and reliable computational tools that allow to simulate the behavior of a ram-air parachute wing. This makes it very difficult to predict the flight ...
    • Design, manufacture, and validation of a student-made ringsail parachute for sounding rocket recovery 

      Britting, Thomas; Joosten, Isabelle; Koops, Bram; Toussaint, Wesley Leonardus Jacobus Rudolf; Sujahudeen, Mohamed Sahir; Vukosavljević, Kristina; Knöll, Niklas Emil; Casablanca, Adriano; Dighe, Nachiket; Scholts, Sebastian Oliver; Kumar, Soham; Van der Wee, Tom (Universitat Politècnica de Catalunya, 2022-04-29)
      Comunicació de congrés
      Accés obert
      In the previous years, the Parachute Research Group (PRG) of Delft Aerospace Rocket Engineering (DARE) has been relying mainly on cruciform, ribbon, or disk-gap-band parachutes for the retrieval of its capsules and smaller ...
    • Estudio de viabilidad técnica del proceso de certificación de paracaídas tácticos Multi-Misión 

      Fradera Arnal, Alex (Universitat Politècnica de Catalunya, 2023-09-15)
      Treball Final de Grau
      Accés restringit per acord de confidencialitat
      Realitzat a/amb:   CIMSA
      Unlike reserve parachutes used in the civilian sector, military tactical parachutes are not subject to any certification standards that guarantee minimum performance criteria. This means that parachutes designed for military ...
    • Ram-air parachute simulation with panel methods and staggered coupling 

      Ortega, Enrique; Flores Le Roux, Roberto Maurice; Pons Prats, Jordi (2016-09-07)
      Article
      Accés obert
    • Selection criteria for parachutes of student-built sounding rockets 

      Britting, Thomas; Toussaint, Wesley Leonardus Jacobus Rudolf; Vukosavljević, Kristina; Sujahudeen, Mohamed Sahir; Knöll, Niklas Emil; Pepermans, Lars; Hadji, Yohan Pascal (Universitat Politècnica de Catalunya, 2022-04-29)
      Comunicació de congrés
      Accés obert
      Various parachute-type decelerators can be considered in the design of a sounding rocket recovery system. During the development of various flagship missions of Delft Aerospace Rocket Engineering (DARE), the Parachute ...
    • Sistema de paracaigudes per a ginys voladors 

      Rivero Prat, Marc (Universitat Politècnica de Catalunya, 2015-07)
      Treball Final de Grau
      Accés obert
      The objective of this project, is to develop a system for deploying a parachute in order to save the integrity of various flying widgets. This project was developed having in mind the idea of saving a drone. This goal wants ...
    • Study and implementation of a control system for autonomous guided parachutes 

      Gutiérrez Meyer, Daniel (Universitat Politècnica de Catalunya, 2018-06-10)
      Treball Final de Grau
      Accés restringit per decisió de l'autor
      1.    Literature review2.    Development of the control routines (PID algorithms) and integration into the simulator.3.    Preliminary verification of the control system.4.    Development and integration of the LL aerodynamic ...
    • Study of a methodology for the flight simulation of ram-air parachutes using a vortex-lattice aerodynamic model 

      Pérez Sánchez, David (Universitat Politècnica de Catalunya, 2017-06-10)
      Treball Final de Grau
      Accés obert
    • Suborbital autorotation landing demonstrator on REXUS 29 

      Mehringer, Johanna; Werner, Lennart; Riegler, Clemens; Dunschen, Frederik (Universitat Politècnica de Catalunya, 2022-04-29)
      Comunicació de congrés
      Accés obert
      Current developments in the aerospace industry point towards more frequent interplanetary travel in the future. However, the main focus of developments is on launcher technology, yet the descent of interplanetary probes ...