The great attention on air-launched microsatellites is due on one hand to the possibilities given by the miniaturization push, making the same performances of traditional satellites achievable with smaller systems, and on the other hand to the disruptive advantages allowed by air-launch techniques, providing Italy not only with an autonomous launch capability, but also with the flexibility to choose the orbit inclination and the launch time, enabling a responsive approach at lower costs respect to ground based launches. In this study, several issues related to this subject are analyzed. A constellation of four microsatellites for electro-optical Earth Observation (EO) is conceived, namely ITAFμSAT (i.e. ITalian Tactical Formation of μ-SATellites). ITAFμSAT is designed to achieve a sub-metric spatial resolution and to offer a high revisit frequency on a specified target area to satisfy military needs. ITAFμSAT is designed to be responsive and the system is conceived to guarantee a fast access to space since the mission is called, through a Plug-and-Play (PnP) approach; to provide Italy with a proprietary system, built, launched and operated on-purpose for its contingent needs; and to complete the information supplied by other EO systems with high quality images captured in a very short time.

Study on an air-launched constellation of tactical micro-satellites for defence Use / R., Cetta; Cecchini, Andrea; F., Capece; P., Gaudenzi. - ELETTRONICO. - (2010), pp. 1-15. (Intervento presentato al convegno Small Satellites Systems and Services - The 4S Symposium 2010 tenutosi a Pestana Conference Centre, Funchal, Madeira (Portugal) nel 31 May - 4 June 2010).

Study on an air-launched constellation of tactical micro-satellites for defence Use

CECCHINI, ANDREA;
2010

Abstract

The great attention on air-launched microsatellites is due on one hand to the possibilities given by the miniaturization push, making the same performances of traditional satellites achievable with smaller systems, and on the other hand to the disruptive advantages allowed by air-launch techniques, providing Italy not only with an autonomous launch capability, but also with the flexibility to choose the orbit inclination and the launch time, enabling a responsive approach at lower costs respect to ground based launches. In this study, several issues related to this subject are analyzed. A constellation of four microsatellites for electro-optical Earth Observation (EO) is conceived, namely ITAFμSAT (i.e. ITalian Tactical Formation of μ-SATellites). ITAFμSAT is designed to achieve a sub-metric spatial resolution and to offer a high revisit frequency on a specified target area to satisfy military needs. ITAFμSAT is designed to be responsive and the system is conceived to guarantee a fast access to space since the mission is called, through a Plug-and-Play (PnP) approach; to provide Italy with a proprietary system, built, launched and operated on-purpose for its contingent needs; and to complete the information supplied by other EO systems with high quality images captured in a very short time.
2010
Study on an air-launched constellation of tactical micro-satellites for defence Use / R., Cetta; Cecchini, Andrea; F., Capece; P., Gaudenzi. - ELETTRONICO. - (2010), pp. 1-15. (Intervento presentato al convegno Small Satellites Systems and Services - The 4S Symposium 2010 tenutosi a Pestana Conference Centre, Funchal, Madeira (Portugal) nel 31 May - 4 June 2010).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/383020
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