RUSSO, ANNAMARIA
RUSSO, ANNAMARIA
DIPARTIMENTO DI INGEGNERIA INDUSTRIALE
Experimental analysis of the fuel regression rate dependence on pressure in a hybrid rocket
2003 Carmicino, C.; Russo, Annamaria
Il Razzo ibrido come propulsore di un aliante
1973 Russo, G. P.; Russo, Annamaria
Evoluzione termofluidodinamica di una miscela liquido-vapore in condizioni di non-equilibrio termodinamico
1981 Russo, G. P.; Russo, Annamaria
Alcuni aspetti della balistica interna di un endoreattore a propellenti ibridi e del comportamento di ugelli a spina troncata”
2004 Russo, Annamaria; Carlomagno, GIOVANNI MARIA
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 Evaluation of the Radiative Heat Flux from Rocket Plumes on Satellite Structures
1983 Monti, R.; Mannara, G.; 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
Numerical simulation of flowfields in a plug nozzle with reacting flow
1999 Russo, Annamaria; D., Paterna; C., Papa
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
On the Role of Vortex Shedding in Hybrid Rockets Combustion Instability
2008 C., Carmicino; Russo, Annamaria
Hybrid-rocket motor performance trade off with paraffin based and metal-loaded HTPB fuel grains
2012 Carmicino, Carmine; Festa, Giandomenico; F., Scaramuzzino; Spiezia, Michele; Russo, Annamaria