Energetic electrons and ions are
magnetically trapped around the Earth forming the radiation belts
, also known
as the Van Allen belts. The radiation belts extend from 100 km to 65 000
km and consist principally of electrons of up to a few MeV energy and protons
of up to several hundred MeV energy. The high energy particle flux in the
radiation belts is dependent on the solar activity. The socalled
Solar Energetic Particles (SEP
) are
high-energy particles that are encountered in interplanetary space and close to
the Earth. These particles are seen in short duration bursts associated with
other solar activity. Solar Energetic Particle Events, as detected in Earth
orbit, can last from a few hours to several days. The Earth’s magnetic field
provides a varying degree of geomagnetic shielding of nearEarth locations from
these particles. They consist of protons, electrons and heavy ions with
energies from a few tens of keV to GeV ranges (the fastest particles can reach
relativistic speeds) and can originate from two processes: energisation in
association with activity seen on the solar disk e.g. flaring, or by shock
waves associated with Coronal Mass Ejection (CMEs) as they propagate through
the heliosphere. They are of particular interest and importance because they
can endanger life and electronics in outer space (especially particles
exceeding some tens of MeV).
Galactic cosmic rays (GCR) are high-energy charged particles that enter the solar system from the outside, the flux of which becomes modulated in anti-correlation with solar activity due to the solar wind. They are composed of protons, electrons, and fully ionized nuclei. There is a continuous and isotropic flux of Galactic Cosmic Ray (GCR) ions. Although the flux is low, a few particles cm-2s-1, GCRs include energetic heavy ions which can deposit significant amounts of energy in sensitive volumes and so cause problems to spacecrafts' electronics and humans in space. As for Solar particles, the Earth’s magnetic field provides a varying degree of geomagnetic shielding of nearEarth locations from these particles.
The Earth’s magnetic field partially shields nearEarth space from solar energetic particles and cosmic rays, an effect known as geomagnetic shielding. However, these particles can easily reach polar regions and high altitudes such as the geostationary orbit. Geomagnetic shielding of protons is computed on the basis of their trajectories in geomagnetic B, L space.
The above environments are common to
planets other than the Earth. Jupiter, Saturn, Uranus and Neptune have strong
magnetic fields inducing severe radiation environments in their radiation
belts
. Mercury has a small magnetosphere which may lead to transient radiation
belts. The other planets (Mars, Venus) have no trapped radiation. Missions to
them are only exposed to GCR and SEP
.
Neutrons are ejected by the Sun. They decay rapidly in the interplanetary medium, and only a few can reach the Earth. They are important for missions close to the Sun.
When highly energetic charged particles strike the earth’s upper atmosphere they create secondary particles throughout the atmosphere including very significant fluxes of neutrons. Of these, some are emitted back into space as atmospheric albedo neutrons of between 0,1 and 2,2 cm-2s-1, depending on the geomagnetic latitude and the phase of the solar cycle, and these are significant for LEO spacecraft including ISS. Model results for albedo neutron spectra are given in Annex I.
For some planetary environments, such as Mars, the secondary neutrons from cosmic ray and solar proton interactions with the atmosphere and regolith become the dominant radiation, in particular for manned missions.
Secondary radiation is generated by the interaction of the above environmental components with materials of the spacecraft. A wide variety of secondary radiations are possible, of varying importance. The ECSS-E-ST-10-12 standard deals with these sources of radiation. Secondary neutrons are important for manned missions and also play a role in generating background in sensitive detector systems.
Other sources of radiation include emissions from onboard radioactive sources such as in instrument calibration units, Radioisotope Thermoelectric Generator (RTG) electrical power systems and Radioisotope Heating Units (RHU). Any use of reactor power sources provide intense fluxes of neutrons and gamma rays.
The above radiation environments represent
important hazards to space missions. Energetic particles, particularly from the
radiation belts
and from solar particle events cause radiation damage to
electronic components, solar cells and materials. They can easily penetrate
typical spacecraft walls and deposit doses of hundreds of kilorads (1 rad = 1
cGy) during missions in certain orbits.
Radiation is a concern for manned missions. The limits of acceptable radiological dose for astronauts, determined to ensure as low as reasonably achievable longterm risk, is indicated in ECSS-E-ST-10-12. There are many possible radiation effects to humans, beyond the scope of this document. These are described in . Heavy ions and neutrons are known to cause severe biological damage, and therefore these contributions receive a heavier weighting than gamma radiation. The “quality factors”, as they are called, are established by the International Commission on Radiological Protection [RD.13].
Energetic ions, primarily from cosmic rays and solar particle events, lose energy rapidly in materials, mainly through ionization. This energy transfer can disrupt or damage targets such as a living cell, or a memory element, leading to Singleevent Effect (SEE) in a component, or an element of a detector (radiation background). These effects can also arise from nuclear interactions between very energetic trapped protons and materials (sensitive parts of components, biological experiments, detectors). Here, the proton breaks the nucleus apart and the fragments cause highlylocalized ionization.
Energetic particles also interfere with payloads, most notably with detectors on astronomy and observation missions where they produce a “background” signal which is not distinguishable from the photon signal being counted, or which can overload the detector system.
Energetic electrons can penetrate thin shields and build up static charge in internal dielectric materials such as cable and other insulation, circuit boards, and on ungrounded metallic parts. These can subsequently discharge, generating electromagnetic interference.
Apart from ionizing dose, particles can lose energy through nonionizing interactions with materials, particularly through “displacement damage”, or “bulk damage”, where atoms are displaced from their original sites. This can alter the electrical, mechanical or optical properties of materials and is an important damage mechanism for electrooptical components (e.g. solar cells and optocouplers) and for detectors, such as CCDs.
For a more complete description of these effects refer to ECSS-E-ST-10-12.