عنوان مقاله [English]
نویسندگان [English]چکیده [English]
According to mission requirements in many of space missions, an exact time should be assigned for launch date namely launch window. Among various parameters influencing launch window, in this article a couple of most mission related ones are being researched. First is some constraints on handling satellite power and the second is the imaging mission constraintsfor a remote sensing satellite. Then after this study on mission requirements a conceptual method for launch window estimation is presented and supported by a case study on sample micro-satellite IRSAT.