ROMANO, MARCELLO
ROMANO, MARCELLO
DIPARTIMENTO DI INGEGNERIA AEROSPAZIALE (attivo dal 01/01/1900 al 31/12/2012)
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Risultati 1 - 6 di 6 (tempo di esecuzione: 0.011 secondi).
A 4-PI steradians dynamic three-axis simulator for satellite hardware-in-the-loop experiments
2013-01-01 Romano, Marcello; Chesi, S.
Active Attitude Control System for Small Spacecraft
2010-01-01 Romano, Marcello; Oppenheimer, P.
Micro-Coupling Active Release Mechanism
2011-01-01 Crane, W.; Oppenheimer, P.; Newman, J.; Romano, Marcello
Micro-Coupling Active Release Mechanism
2013-01-01 Crane, W.; Oppenheimer, P.; Newman, J.; Romano, Marcello
Novel Electrical Thruster for Small Spacecraft
2011-01-01 Biblarz, O.; Romano, Marcello; Oppenheimer, P.
Spacecraft Docking Interface Mechanism
2010-01-01 Romano, Marcello; Oppenheimer, P.
| Titolo | Data di pubblicazione | Autori | File |
|---|---|---|---|
| A 4-PI steradians dynamic three-axis simulator for satellite hardware-in-the-loop experiments | 1-gen-2013 | ROMANO, MARCELLO + | |
| Active Attitude Control System for Small Spacecraft | 1-gen-2010 | ROMANO, MARCELLO + | |
| Micro-Coupling Active Release Mechanism | 1-gen-2011 | ROMANO, MARCELLO + | |
| Micro-Coupling Active Release Mechanism | 1-gen-2013 | ROMANO, MARCELLO + | |
| Novel Electrical Thruster for Small Spacecraft | 1-gen-2011 | ROMANO, MARCELLO + | |
| Spacecraft Docking Interface Mechanism | 1-gen-2010 | ROMANO, MARCELLO + |