Joan Pau Sanchez Cuartielles
Joan Pau Sanchez Cuartielles
Lecturer in Space Engineering, Cranfield University, Cranfield (UK).
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TitleCited byYear
Low-energy, low-thrust transfers to the Moon
G Mingotti, F Topputo, F Bernelli-Zazzera
Celestial Mechanics and Dynamical Astronomy 105 (1-3), 61, 2009
Multicriteria comparison among several mitigation strategies for dangerous near-earth objects
P Sanchez, C Colombo, M Vasile, G Radice
Journal of Guidance, Control, and Dynamics 32 (1), 121-142, 2009
Easily retrievable objects among the NEO population
DG Yárnoz, JP Sánchez, CR McInnes
Celestial Mechanics and Dynamical Astronomy 116 (4), 367-388, 2013
Asteroid resource map for near-Earth space
JP Sanchez, C McInnes
Journal of Spacecraft and Rockets 48 (1), 153-165, 2011
Comparison of single and multi‐spacecraft configurations for NEA deflection by solar sublimation
C Maddock, JP Sanchez Cuartielles, M Vasile, G Radice
AIP conference Proceedings 886 (1), 303-316, 2007
Assessment on the feasibility of future shepherding of asteroid resources
JP Sanchez, CR McInnes
Acta Astronautica 73, 49-66, 2012
Impact hazard protection efficiency by a small kinetic impactor
JP Sanchez, C Colombo
Journal of Spacecraft and Rockets 50 (2), 380-393, 2013
On the consequences of a fragmentation due to a NEO mitigation strategy
JP Sanchez, M Vasile, G Radice
Synergistic approach of asteroid exploitation and planetary protection
JP Sanchez, CR McInnes
Advances in Space Research 49 (4), 667-685, 2012
On the ballistic capture of asteroids for resource utilization
JP Sanchez, CR McInnes
62nd International Astronautical Congress 1, 1-16, 2011
The feasibility of using an L1 positioned dust cloud as a method of space-based geoengineering
R Bewick, JP Sanchez, CR McInnes
Advances in Space Research 49 (7), 1212-1228, 2012
A Multi‐criteria assessment of deflection methods for dangerous NEOs
JP Sanchez Cuartielles, C Colombo, M Vasile, G Radice
AIP conference proceedings 886 (1), 317-336, 2007
Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun–Earth circular restricted three-body problem
G Mingotti, JP Sánchez, CR McInnes
Celestial mechanics and dynamical astronomy 120 (3), 309-336, 2014
Asteroid retrieval missions enabled by invariant manifold dynamics
JP Sanchez, DG Yárnoz
Acta Astronautica 127, 667-677, 2016
Effects of NEO composition on deflection methodologies
Y Sugimoto, G Radice, JP Sanchez
Acta Astronautica 90 (1), 14-21, 2013
The Castalia mission to main belt comet 133p/Elst-Pizarro
C Snodgrass, GH Jones, H Böhnhardt, A Gibbings, M Homeister, N Andre, ...
Advances in space research 62 (8), 1947-1976, 2018
Gravitational capture opportunites for asteroid retrieval missions
JP Sanchez Cuartielles, D Garcia Yarnoz, EM Alessi, C McInnes
63rd International Astronautical Congress, 2012
A comparative assessment of different deviation strategies for dangerous NEO
C Colombo, JP S Cuartielles, M Vasile, G Radice
AIAA 57th International Astronautical Congress, AC-06-A3. 5.8, 2006
Control of asteroid retrieval trajectories to libration point orbits
M Ceriotti, JP Sanchez
Acta Astronautica 126, 342-353, 2016
Light-touch2: a laser-based solution for the deflection, manipulation and exploitation of small asteroids
M Vasile, M Vetrisano, A Gibbings, D Garcia Yarnoz, ...
IAA Planetary Defense Conference, Paper IAA-PDC13-04-22, 2013
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