Problema de Sitnikov

Autor: Quera Coderch, Lı́dia

Treballs Finals de Grau de Matemàtiques, Facultat de Matemàtiques, Universitat de Barcelona, Any: 2023, Director: Ernest Fontich
[en] The Sitnikov Problem is the study of the dynamics of a particular system in the restricted Three-Body Problem

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od_______963::81f5a0cc38e14b5d61b26d7819abc243
http://hdl.handle.net/2445/199100

A Method for the Experimental Characterisation of Novel Drag-Reducing Materials for Very Low Earth Orbits using the Satellite for Orbital Aerodynamics Research (SOAR) Mission

Autor: Nicholas H. Crisp, Peter C. E. Roberts, Virginia Hanessian, Valeria Sulliotti-Linner, Georg H. Herdrich, Daniel García-Almiñana, Dhiren Kataria, Simon Seminari

Publikováno v: Crisp, N H, Roberts, P C E, Hanessian, V, Sulliotti-Linner, V, Herdrich, G H, Garcia-Alminana, D, Kataria, D & Seminari, S 2022, ' A Method for the Experimental Characterisation of Novel Drag-Reducing Materials for Very Low Earth Orbits using the Satellite for Orbital Aerodynamics Research (SOAR) Mission ', CEAS Space Journal . https://doi.org/10.1007/s12567-022-00434-3
UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)

The Satellite for Orbital Aerodynamics Research (SOAR) is a 3U CubeSat mission that aims to investigate the gas–surface interactions (GSIs) of different materials in the very low Earth orbit environment (VLEO), i.e. below 450 km. Improving the unde

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6439e5c61e3c113d3b6c58088cdcd4dc
https://www.research.manchester.ac.uk/portal/en/publications/a-method-for-the-experimental-characterisation-of-novel-dragreducing-materials-for-very-low-earth-orbits-using-the-satellite-for-orbital-aerodynamics-research-soar-mission(fa12ef12-91b5-4422-8c80-3a53589d75f8).html

Feasibility study of the CASTOR Mission for small space debris in situ monitoring

Autor: Busquets Soler, Lluc-Ramon

Publikováno v: UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)

Aquest treball presenta l'estudi numèric de viabilitat de l'arquitectura de missió proposada per l'equip 4DCube de l'IEEC per a monitorització in situ de fragments petits de brossa espacial (

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::3ca30bbfb291db8c062b797c6d6e5e98
https://hdl.handle.net/2117/360519

Study and evaluation of the performance of a multistage solid-propellant rocket vehicle, including atmospheric ascent and orbital insertion

Autor: Vergés Eiras, Roger

Publikováno v: UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)

En aquest projecte s'estudia i s'avalua el rendiment d'un coet de diverses etapes de propel·lent sòlid durant tot el seu ascens atmosfèric i fins a la seva inserció orbital. Per tant, en primer lloc s'analitza la composició química del fuel i l

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::f4a599ee8b56afd8e3948278ff39859d
http://hdl.handle.net/2117/360875

Leveraging L3 to transfer to L4 in the Sun-perturbed Earth-Moon system

Autor: Àngel Jorba, Begoña Nicolás, Yuying Liang

Publikováno v: Dipòsit Digital de la UB
Universidad de Barcelona

This paper is devoted to a new approach to construct the transfers from the Earth to the Earth-Moon (EM) $L_{4}$ using stable and unstable manifolds of planar quasiperiodic Lyapunov orbits (QPLOs) of the EM $L_{3}$ in the planar bicircular SunEarth-M

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::46f83a8948e15ef2f8f921f2476d35b7
http://hdl.handle.net/2445/183530