آئی ایس ایس این نمبر
تازہ ترین جلد
In general estimated constant drag coefficient is used for the dynamic modeling of satellites in an orbit. This causes uncertainties in the prediction of satellite orbital perturbations. In the pas ... Read More
In this paper we describe derivation of a new iterative method for solving nonlinear equations. The method is shown to have convergence order five. Furthermore we show that the convergence order ma ... Read More
The majority of space objects now being launched into orbit come from a class of space objects that fall under the heading of small satellites. This category typically includes all satellites under ... Read More
This paper efforts to review the potential uses of Composite materials in Space industry. Composite materials have revolutionized the space industry by virtue of their multifunctional, multi-directi ... Read More
In this study, the suitability of the research version Tropical Rainfall Measuring Mission (TRMM) Multi-satellite Precipitation Analysis (TMPA) 3-hourly product has been evaluated at various time s ... Read More
Post-industrial revolution led to the emergence of Reconfigurable Manufacturing Systems as result of increasing market and manufacturing demands. Shorter product life-cycle, competitive pricing, di ... Read More
Welding response of two advanced aluminiumlithium (Al-Li) alloys was studied in terms of metallurgical and mechanical properties. The first alloy Al-Li 2195 contains Li metal by weight ~1.1%, wherea ... Read More
Effect due to ageing time and stress on the corrosion behavior of Aluminum-Coper alloy AA 2024-T6 is studied. The alloy specimens were aged for 6 hrs, 9 hrs and 12 hrs ageing time and then subjecte ... Read More
During ascent of space launch vehicle in atmosphere, the payload compartment pressure should be leveled with the atmospheric pressure. At high altitudes, this pressure difference becomes more destr ... Read More
This paper presents the active control scheme for buffet load attenuation on the wings of advanced commercial aircraft prototype, built under (3AS) European project in Politecnico di Milano. Finite ... Read More
Due to the hostile nature of the space environment, fault tolerance has become a key part of recent research in spacecraft mission planning. Spacecraft are complex systems; mission planning in spac ... Read More
Satellites are subject to various severe vibration during different phases of flight. The concept of satellite smart adapter is proposed in this study to achieve active vibration control of launch ... Read More