RUSSO, ANNAMARIA
RUSSO, ANNAMARIA
DIPARTIMENTO DI INGEGNERIA INDUSTRIALE
The role of injection in the hybrid rockets regression rate behaviour
2005 Carmicino, Carmine; Russo, Annamaria
The Pressure Sensitivity of the Ultrasonic Waves Velocity: a Contribution to a Better Determination of the Energetic Material Regression Rate
2005 F., Cauty; C., Carmicino; Russo, Annamaria
Experimental tests on a lab-scale hybrid rocket
2001 Russo, Annamaria; Carmicino, C.; Ferrazzano, L.; Capasso, C.
Design of a lab- scale cooled two-dimensional plug nozzle for experimental tests
2002 Russo, Annamaria; Carmicino, C.; Nocito, A.
Modelling hydrogen peroxide decomposition in monolithic beds
2006 Bonifacio, S; Russo, Annamaria
Investigation on the Fuel Regression Rate Dependence on oxidizer Injection and Chamber Pressure in a Hybrid Rocket
2003 Carmicino, C.; Russo, Annamaria
The Effects of Oxidizer Injector Design on Hybrid Rockets Combustion Stability
2006 Carmicino, C; Russo, Annamaria
Operational Research Project on Hybrid Engine in Europe
2008 Russo, Annamaria
The Pressure Sensitivity of the Ultrasonic Waves Velocity: a Contribution to a Better Determination of the Energetic Material Regression Rate
2007 F., Cauty; Carmicino, Carmine; Russo, Annamaria
Hybrid Propellants Gas Generator
1999 Russo, Annamaria
Design and Preliminary tests of a HTP/HDPE hybrid rocket for de-orbit manoeuvring
2003 Boffa, N. D.; Carmicino, C.; Pilone, G.; Russo, Annamaria
Hybrid Rocket as an Active System for Satellites De-Orbiting
2010 Carmicino, Carmine; Russo, Annamaria
The Oxidiser Injection in Hybrids: a Means to Control Motor Performance
2006 Carmicino, C; Russo, Annamaria
Advanced Solid Fuels for Hybrid Propulsion: the Research Activity in Europe
2011 Carmicino, Carmine; Russo, Annamaria; O., Orlandi; H., Blanchard; P., Yvart; P., Gautier
The influence of a conical axial injector on hybrid rockets performance
2005 C., Carmicino; Russo, Annamaria
Performance comparison between two different injector configurations in a hybrid rocket
2005 C., Carmicino; Russo, Annamaria
An optimum configuration of a completely reusable vehicle for LEO missions
1999 Russo, Annamaria; Stia, G.; Bove, M.
Lubrificazione Idrodinamica Non-Newtoniana. Soluzione numerica con gli elementi finiti
1976 Golia, C.; Russo, Annamaria
Misure di spinta e visualizzazione del campo di flusso di ugelli a spina
1999 Onofri, M.; Russo, Annamaria; Zannetti, L.
Decomposition of hydrogen peroxide on MnO2/TiO2 catalysts
2004 Russo, Annamaria; Turco, Maria; G., Pilone; Bagnasco, Giovanni
| Titolo | Tipologia | Data di pubblicazione | Autore(i) | File |
|---|---|---|---|---|
| The role of injection in the hybrid rockets regression rate behaviour | 1.1 Articolo in rivista | 2005 | Carmicino, Carmine; Russo, Annamaria | |
| The Pressure Sensitivity of the Ultrasonic Waves Velocity: a Contribution to a Better Determination of the Energetic Material Regression Rate | 4.1 Articoli in Atti di convegno | 2005 | F., Cauty; C., Carmicino; Russo, Annamaria | |
| Experimental tests on a lab-scale hybrid rocket | 4.1 Articoli in Atti di convegno | 2001 | Russo, Annamaria; Carmicino, C.; Ferrazzano, L.; Capasso, C. | |
| Design of a lab- scale cooled two-dimensional plug nozzle for experimental tests | 4.1 Articoli in Atti di convegno | 2002 | Russo, Annamaria; Carmicino, C.; Nocito, A. | |
| Modelling hydrogen peroxide decomposition in monolithic beds | 4.1 Articoli in Atti di convegno | 2006 | Bonifacio, S; Russo, Annamaria | |
| Investigation on the Fuel Regression Rate Dependence on oxidizer Injection and Chamber Pressure in a Hybrid Rocket | 4.1 Articoli in Atti di convegno | 2003 | Carmicino, C.; Russo, Annamaria | |
| The Effects of Oxidizer Injector Design on Hybrid Rockets Combustion Stability | 4.1 Articoli in Atti di convegno | 2006 | Carmicino, C; Russo, Annamaria | |
| Operational Research Project on Hybrid Engine in Europe | 8.07 Progetti di Ricerca Finanziati | 2008 | Russo, Annamaria | |
| The Pressure Sensitivity of the Ultrasonic Waves Velocity: a Contribution to a Better Determination of the Energetic Material Regression Rate | 1.1 Articolo in rivista | 2007 | F., Cauty; Carmicino, Carmine; Russo, Annamaria | |
| Hybrid Propellants Gas Generator | 4.1 Articoli in Atti di convegno | 1999 | Russo, Annamaria | |
| Design and Preliminary tests of a HTP/HDPE hybrid rocket for de-orbit manoeuvring | 4.1 Articoli in Atti di convegno | 2003 | Boffa, N. D.; Carmicino, C.; Pilone, G.; Russo, Annamaria | |
| Hybrid Rocket as an Active System for Satellites De-Orbiting | 4.1 Articoli in Atti di convegno | 2010 | Carmicino, Carmine; Russo, Annamaria | |
| The Oxidiser Injection in Hybrids: a Means to Control Motor Performance | 4.1 Articoli in Atti di convegno | 2006 | Carmicino, C; Russo, Annamaria | |
| Advanced Solid Fuels for Hybrid Propulsion: the Research Activity in Europe | 4.1 Articoli in Atti di convegno | 2011 | Carmicino, Carmine; Russo, Annamaria; O., Orlandi; H., Blanchard; P., Yvart; P., Gautier | |
| The influence of a conical axial injector on hybrid rockets performance | 4.1 Articoli in Atti di convegno | 2005 | C., Carmicino; Russo, Annamaria | |
| Performance comparison between two different injector configurations in a hybrid rocket | 4.1 Articoli in Atti di convegno | 2005 | C., Carmicino; Russo, Annamaria | |
| An optimum configuration of a completely reusable vehicle for LEO missions | 1.1 Articolo in rivista | 1999 | Russo, Annamaria; Stia, G.; Bove, M. | |
| Lubrificazione Idrodinamica Non-Newtoniana. Soluzione numerica con gli elementi finiti | 1.1 Articolo in rivista | 1976 | Golia, C.; Russo, Annamaria | |
| Misure di spinta e visualizzazione del campo di flusso di ugelli a spina | 8.07 Progetti di Ricerca Finanziati | 1999 | Onofri, M.; Russo, Annamaria; Zannetti, L. | |
| Decomposition of hydrogen peroxide on MnO2/TiO2 catalysts | 1.1 Articolo in rivista | 2004 | Russo, Annamaria; Turco, Maria; G., Pilone; Bagnasco, Giovanni |