Passivation (spacecraft)
Removal of internal energy in a spaceship at end of its mission From Wikipedia, the free encyclopedia
Removal of internal energy in a spaceship at end of its mission From Wikipedia, the free encyclopedia
The passivation of a spacecraft is the removal of any internal energy contained in the vehicle at the end of its mission or useful life.[1] Spent upper stages are generally passivated after their use as launch vehicles is complete, as are satellites when they can no longer be used for their design purpose.
Internally stored energy generally takes the form of unused propellant[1] and batteries.[2] In the past, such stored energy has sometimes led to fragmentation or explosion, producing unwanted space debris.[1][2] This was a fairly common outcome for many of the U.S.[3] and Soviet rocket designs from the 1960s to the 1980s.[4] It remains an occasional problem with derelict second stages left in higher Earth orbits; several U.S. rocket stages fragmented in 2018 and 2019.
The International Telecommunication Union (ITU) and United Nations (UN) recommend that satellites in geosynchronous orbit be designed to move themselves to a disposal orbit some 350 kilometres (220 mi) above the GEO belt, and then remove internally stored energy. Most GEO satellites conform to these recommendations, although there are no enforcement mechanisms.[1]
Within national regimes, where national governments can control the launch licenses of launch vehicles and spacecraft, there are some enforceable requirements for passivation.
The U.S. government has a set of standard practices for civilian (NASA) and military (DoD/USSF) orbital debris mitigation that require passivation for space launches with U.S. launch licenses. "All on-board sources of stored energy of a spacecraft or upper stage should be depleted or safed when they are no longer required for mission operations or postmission disposal. Depletion should occur as soon as such an operation does not pose an unacceptable risk to the payload. Propellant depletion burns and compressed gas releases should be designed to minimize the probability of subsequent accidental collision and to minimize the impact of a subsequent accidental explosion."[5][6]
Passivation practice on many launches in recent decades has not mitigated second-stage breakups. Upper stage deflagration/breakup events have continued even with newer rocket designs of the 2010s, long after the negative externality of space debris became widely considered as a much larger social problem. For example, there were three upper-stage breakups in just the late 2010s:
