Chemical and Radiative Size—Related Effects on the Performance of Liquid Rocket Engines fed with Different Propellant Combinations D. Lentini OriginalPaper 01 April 2015 Pages: 73 - 80
Status and Perspectives of Hypersonic Systems and Technologies with Emphasis on the Role of Sub-Orbital Flight S. ChiesaG. RussoS. Corpino OriginalPaper 01 April 2015 Pages: 81 - 90
A Hybrid Formulation for Modelling Multibody Spacecraft A. PisculliL. FelicettiG. B. Palmerini OriginalPaper 01 April 2015 Pages: 91 - 101
MISTRAL: Air-Launchable Micro-Satellite with Re-Entry Capability R. FortezzaR. SavinoG. Russo OriginalPaper 01 April 2015 Pages: 102 - 112
Aerodynamic design of a light amphibious PrandtlPlane: wind tunnel tests and CFD validation V. CipollaA. FredianiF. Oliviero OriginalPaper 01 April 2015 Pages: 113 - 123
Development of finite element model for morphing inflatable winglet A. De FenzaD. D’OrazioL. Lecce OriginalPaper 01 April 2015 Pages: 124 - 132
Finite Element Analysis of Thermoelectric-Galvanomagnetic interactions and their aerospace applications Said Abouali Sánchez Paper from Euroavia students 01 April 2015 Pages: 133 - 135