The retirement of a spacecraft refers to the discontinuation of a spacecraft from active service. This can involve deorbiting the spacecraft, discontinuing the probes operations, passivating, or loss of contact with it. One notable example of spacecraft retirement is Cassini's retirement in 2017.
History The first spacecraft to be retired was the Soviet Union's Sputnik 1 probe. Launched in 1957, Sputnik 1 completed its mission when it naturally deorbited due to atmospheric drag after approximately three months in orbit, completing a total of 1,440 orbits around Earth. In 1958, NASA launched the Vanguard 1 probe as part of its efforts in the Space Race. Six years later, NASA officially concluded the mission as the probe had fulfilled all its experimental and objective requirements. Initially, NASA estimated that Vanguard 1 would remain in low Earth orbit for up to 2,000 years. However, due to solar radiation pressure and atmospheric drag, this estimate has been revised. Vanguard 1 is now expected to re-enter Earth's atmosphere and burn up in approximately 240 years. Following the discontinuation of the Vanguard 1 probe, many space agencies and subsequent spacecraft have ceased operations through various methods. In 2017, the Cassini–Huygens probe concluded its 19-year exploration mission by descending into Saturn's atmosphere. The decision to end the mission was prompted by the minimal power supply remaining in the probe's radioisotope thermoelectric generators (RTGs). The maneuver began on November 29, 2016, when Cassini performed a flyby of Saturn's moon Titan, positioning it into the orbital plane of Saturn's F Ring for its grand finale. Cassini conducted another flyby of Titan on April 22, 2017, positioning the probe to pass within a precise 3,100 km (1,900 mi) of Saturn's clouds. This maneuver was repeated 22 times until September 15, 2017, at 11:55:46 UTC, when communication with Cassini's high-gain antenna was lost during the final flyby of Saturn. Cassini's grand finale represented the first intentional entry of a spacecraft into the atmosphere of a gas giant and marked the first major spacecraft to burn up in such an atmosphere. The mission's success has significantly influenced the planning and execution of both current and future missions focused on gas and ice giants. In the beginning of the 21st century retirement is not yet a routine end-of-mission process for the geostationary satellites.
Reasons
Exhaustion of propellant The satellites expend their propellant for the orbital station-keeping and eventually run out of it. For the high-value satellites in the geostationary orbit, the amount of the onboard propellant is usually the limiting factor of their service life (12-15 years at the beginning of the 21st century).
Power decrement
Many modern spacecraft utilize radioisotope thermoelectric generators (RTGs), and spacecraft electric propulsion as their power source. Over time, the power output of RTGs or SEPs diminishes due to the gradual depletion of the radioactive isotopes they rely on for electricity generation. Radioisotope thermoelectric generators convert the heat generated by the decay of radioactive isotopes into electricity. As the radioactive isotopes decay over time, the power output of the RTGs gradually decreases. It's estimated that the power output from the RTGs will fall below the threshold required to operate the spacecraft's systems effectively, including communication with Earth and scientific instruments. As a result, spacecraft equipped with RTGs will eventually have insufficient power to run their instruments. Spacecraft electric propulsion systems utilize electric fields to accelerate charged ions to high velocities, generating thrust for propulsion. Unlike chemical propulsion systems, which rely on the combustion of propellant, electric propulsion systems ionize propellant using electrical energy and then accelerate the resulting ions to produce thrust. As the ions are expelled from the spacecraft at high speeds, they create thrust in the opposite direction, enabling spacecraft maneuverability. Electric propulsion systems offer high efficiency and long-duration capabilities, making them suitable for precise trajectory adjustments, extended deep space missions, and potential future crewed missions. These systems rely on electrical energy for ionization and acceleration of propellant, typically supplied by onboard power sources such as solar panels or batteries. However, over time, these energy sources may become depleted, particularly in missions with extended durations or in environments with limited sunlight. Additionally, the components of SEP systems, including power electronics and ionization chambers, may degrade due to exposure to space conditions, leading to decreased efficiency and power output. Some SEP systems have a limited supply of propellant, such as xenon gas, which can be exhausted over the course of a mission, rendering the system unable to generate thrust. The end of a spacecraft's mission or operational life may also result in the cessation of power generation by the SEP system, marking the conclusion of its propulsion capabilities.
Degradation of instruments
Spacecraft instruments are susceptible to various external factors, including solar wind and other space phenomena. Solar wind, consisting of charged particles emitted by the Sun, can disrupt sensitive instruments like magnetometers and particle detectors, potentially reducing sensitivity or causing complete loss of functionality. Other space phenomena, such as cosmic rays and micrometeoroid impacts, also pose risks, potentially damaging spacecraft components and degrading instrument performance over time. Additionally, temperature extremes and outgassing of materials in space can further impact instrument functionality.
Loss of contact
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