Author/Authors :
Ik Jun Jang، نويسنده , , Hye Sun Shin، نويسنده , , Na Ra Shin، نويسنده , , Su Hyun Kim، نويسنده , , Su Kyum Kim، نويسنده , , Myoung Jong Yu، نويسنده , , Sung-June Cho، نويسنده ,
Abstract :
Decomposition of hydrazine allows the attitude and altitude control of satellite. Macroporous–mesoporous alumina supported iridium catalyst (KCMC-7) has been developed using the fast dehydration of aluminium trihydroxide and subsequent multiple impregnations. The result of data analysis suggested that the obtained alumina was ρ-Al2O3 with both macro and mesopores. Significant amount of pentagonal Al sites after rehydration of ρ-Al2O3 was responsible for ultra high dispersion for ultra high loading of metal around 30 wt%. The performance of the KCMC-7 measured using 4.5 N dual thruster module was satisfactory until the end of life, providing enough thrust for the attitude and altitude control of satellite in the pressure range of 50–350 psi.
Keywords :
Hydrazine decomposition , Satellite , ?-alumina , Ir nanoparticles