| Optimum design of ablative thermal protection systems for atmospheric entry vehicles A Riccio, F Raimondo, A Sellitto, V Carandente, R Scigliano, D Tescione Applied Thermal Engineering 119, 541-552, 2017 | 94 | 2017 |
| Thermo-structural behaviour of an UHTC made nose cap of a reentry vehicle R Borrelli, A Riccio, D Tescione, R Gardi, G Marino Acta Astronautica 65 (3-4), 442-456, 2009 | 78 | 2009 |
| Delamination buckling and growth phenomena in stiffened composite panels under compression. Part I: An experimental study A Riccio, A Raimondo, S Fragale, F Camerlingo, B Gambino, C Toscano, ... Journal of Composite Materials 48 (23), 2843-2855, 2014 | 48 | 2014 |
| The USV Program &UHTC Development G Russo, G Marino Hot Structures and Thermal Protection Systems for Space Vehicles 521, 29, 2003 | 29 | 2003 |
| Numerical/experimental correlation of a plasma wind tunnel test on a UHTC-made nose cap of a reentry vehicle R Borrelli, A Riccio, D Tescione, R Gardi, G Marino Journal of Aerospace Engineering 23 (4), 309-316, 2010 | 25 | 2010 |
| Thermostructural design of a flying winglet experimental structure for the EXPERT re-entry test M Ferraiuolo, A Riccio, M Gigliotti, D Tescione, R Gardi, G Marino | 20 | 2009 |
| Contact sensitivity analysis of a coupling pin for the nose cap of a launch re-entry vehicle M Ferraiuolo, A Riccio, D Tescione, R Gardi, G Marino 57th International Astronautical Congress, C2. 1.08, 2008 | 13 | 2008 |
| The Vibrational-Translational Relaxation of CF2HCl in Ar V Tosa, R Bruzzese, C de Lisio, D Tescione Laser Chemistry 15, 47-54, 1994 | 12* | 1994 |
| Numerical Simulations of Inter-laminar damage evolution in a composite wing box A Riccio, A Raimondo, R Borrelli, U Mercurio, D Tescione, ... Applied Composite Materials 21, 467-481, 2014 | 10 | 2014 |
| Damage tolerance evaluation of a C/C-SiC composite body flap of a re-entry vehicle F Di Caprio, A Russo, C Manservigi, R Scigliano, MDS Fumo, D Tescione, ... Composite Structures 274, 114341, 2021 | 9 | 2021 |
| A Multidisciplinary Approach for the Analysis of Heat Shielded Space Structures GC Rufolo, D Tescione, S Borrelli Hot Structures and Thermal Protection Systems for Space Vehicles 521, 231, 2003 | 7 | 2003 |
| A Fast Procedure For Optimizing Thermal Protection Systems Of Re-Entry Vehicles M Ferraiuolo, A Riccio, D Tescione, M Gigliotti Journal of the British Interplanetary Society 61 (12), 478, 2008 | 4 | 2008 |
| New Materials and Related Fabrication Processes for Hot Structures on RLV's G Marino 54th International Astronautical Congress of the International Astronautical …, 2003 | 4 | 2003 |
| Design optimization of interfacing attachments for the deployable wing of an unmanned re-entry vehicle F Di Caprio, R Scigliano, R Fauci, D Tescione Algorithms 14 (5), 141, 2021 | 2 | 2021 |
| Numerical and Experimental Study of Defects Evolution in a Composites Wing Box Under Compressive Loads R Borrelli, U Mercurio, D Tescione, B Gambino, A Riccio Proceedings of the NATO AVT-211 Workshop on “Understanding Failure …, 2013 | 1 | 2013 |
| A new technique for calibration in frequency of piezoelectric transducers D Tescione, P Maddalena NDT & E International 32 (2), 71-77, 1999 | 1 | 1999 |
| Numerical and Experimental Study of Defects Evolution in a Composites Wing Box Under Compressive Loads B Gambino, R Borrelli, U Mercurio, D Tescione, A Riccio | | 2013 |
| Thermo Mechanical Design Methodologies M Ferraiuolo, C Sellitto, A Riccio, D Tescione Proceedings of the first Workshop on Science and Technology of UHTC-based …, 2009 | | 2009 |
| Study of a coupling mechanism between two bodies at high temperature values M Ferraiuolo, R Borrelli, A Riccio, R Gardi, D Tescione, G Marino 59th International Astronautical conference–IAC 2008 Proceedings 8, 5271-5280, 2008 | | 2008 |
| A Stochastic Approach to the Damage Resistance Analysis of Stiffened Composite Panels C Sellitto, A Riccio, D Tescione Proceedings of the Ninth International Conference on Computational …, 2008 | | 2008 |
