Small spacecraft may carry out surveillance of crisis areas in an effective way when deployed in constellations. In order to limit cost, small spacecraft shall operate at low orbital altitude, so as to use small and relatively unexpensive optical payloads. We show that extended operation in low LEO is made possible by the use of electric propulsion for atmospheric drag compensation. Mission performance is discussed with reference to utilization for the surveillance of a Mediterranean/Middle East region with an extended mission target lifetime of up to 8 years. The constellation design and the overall spacecraft arrangement are presented, as well as the electric propulsion subsystem, based on the HT100 Hall thruster by Alta
The operation of satellites in very low Earth orbit (VLEO) has been linked to a variety of benefits ...
The extension of highly elliptical orbits, with free selection of orbit period, using low thrust pro...
Air-breathing electric propulsion (ABEP) enables long duration missions at very low orbital altitude...
The paper presents the study of a microsatellites constellation equipped with electric thrusters to ...
The recent explosion in proposed microsatellite missions is based on the possibility to mass-produce...
We present a constellation of three satellites capable of remote sensing operation at an orbital alt...
Earth observation is one of the most important satellites' applications. Past earth observation syst...
Small platforms represent valuable options for small scientific and Earth observation missions. One ...
Very Low Earth Orbits (VLEOs), those below 450 km, present a number of benefits and challenges for t...
Small Earth Observation satellites can obtain higher resolution with smaller payloads when operating...
An approach of using a very low flying orbit for a microsatellite to achieve a low cost imaging miss...
In recent years, thanks to advancements in commercial hardware technology miniaturization, small sat...
Small Earth Observation satellites can obtain higher resolution with smaller payloads when operating...
The use of extended static-highly elliptical orbits, termed Taranis orbits, is considered for contin...
Low thrust electric propulsion systems find a promising application field on small-to-medium sized s...
The operation of satellites in very low Earth orbit (VLEO) has been linked to a variety of benefits ...
The extension of highly elliptical orbits, with free selection of orbit period, using low thrust pro...
Air-breathing electric propulsion (ABEP) enables long duration missions at very low orbital altitude...
The paper presents the study of a microsatellites constellation equipped with electric thrusters to ...
The recent explosion in proposed microsatellite missions is based on the possibility to mass-produce...
We present a constellation of three satellites capable of remote sensing operation at an orbital alt...
Earth observation is one of the most important satellites' applications. Past earth observation syst...
Small platforms represent valuable options for small scientific and Earth observation missions. One ...
Very Low Earth Orbits (VLEOs), those below 450 km, present a number of benefits and challenges for t...
Small Earth Observation satellites can obtain higher resolution with smaller payloads when operating...
An approach of using a very low flying orbit for a microsatellite to achieve a low cost imaging miss...
In recent years, thanks to advancements in commercial hardware technology miniaturization, small sat...
Small Earth Observation satellites can obtain higher resolution with smaller payloads when operating...
The use of extended static-highly elliptical orbits, termed Taranis orbits, is considered for contin...
Low thrust electric propulsion systems find a promising application field on small-to-medium sized s...
The operation of satellites in very low Earth orbit (VLEO) has been linked to a variety of benefits ...
The extension of highly elliptical orbits, with free selection of orbit period, using low thrust pro...
Air-breathing electric propulsion (ABEP) enables long duration missions at very low orbital altitude...