… at the end of the mission. This section introduces the … FORESAIL-1 mission: measurements
of energetic particle precipitation and solar energetic neutral atoms (ENAs), and deorbiting …

… demonstrate a satellite de-orbiting 47 technology, and for the first time, make an orbit manoeuvre
with a propellantless nanosatel48 lite. FORESAIL-1 will demonstrate … radiation belt loss …

… Foresail-1 mission Figure 1 is to measure charged particle precipitation and to demonstrate
an electrostatic deorbiting … Unfortunately, after two weeks the satellite was lost due to …

… of the radiation belts with its satellite mission Foresail-2. The … to accurately quantify their
contribution to electron losses. … the proposed radiation shield and to demonstrate that COTS …

… for deorbiting in LEO on two upcoming cubesat missions – … –90% so that the electron losses
at the extractor remain small. … modes and to demonstrate deorbiting with the plasma brake. …

… radiation belts as a function of energy, time and pitch angle. In addition to measuring the
electrons in outer radiation belt … Figure 25, shows that the temperature profile is similar to the hot …

… radiation belts: FORESAIL-1 is the first nano-satellite mission … can deorbit actively, our
deorbiting scheme adopts passive … and loss mechanism of high-energy electrons in the radiation …

… FORESAIL-1 mission has two objectives consisting of measuring radiation belt losses
alongside with demonstrating the feasibility of de-orbiting a CubeSat in LEO using plasma brake …

… of radiation belt losses and demonstrate deorbiting in LEO. … about FORESAIL missions
which is another cubesat mission … satellite’s linear velocity to find the final torque affecting the …

… for attenuation in a satellite link is the free space path loss (FSPL). It … The mission of Foresail-1
satellite is to investigate electron … environment and a plasma brake (PB) for deorbiting. The …