... missions to perform deorbiting manoeuvres, and hence self-deorbiting is often not possible. As such, ADR by means of remover spacecraft seems to be inevitable. In the net removal method a net is deployed towards the target which is captured and then...
... mass of 800kg – less than a third of Rosetta’s launch mass. Measuring 1.8 x 2.0 x 2.1m across with solar arrays stowed, the spacecraft design is a simple one with fixed solar arrays, a fixed high-gain antenna and a bipropellant propulsion system...
... as a failure by the fault detection and recovery logic. Also the whole swing-by scenario had to be re-designed to establish a spacecraft configuration that would minimise power consumption whilst in the shadow. It was not an easy task but we had...
... life?’ The JUICE payload consists of 10 state-of-the-art instruments plus one experiment that uses the spacecraft telecommunication system with ground-based telescopes. This payload, summarised in Table 1, is capable of addressing all of the mission...