2014
DOI: 10.1016/j.asr.2014.09.012
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Highly Elliptical Orbits for Arctic observations: Assessment of ionizing radiation

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Cited by 15 publications
(19 citation statements)
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“…By selecting the inclination of the orbit to situate the apogee near the critical inclination of 63.44°N, a single satellite can make quasi‐geostationary observations of the ABZ for a limited time before accelerating toward perigee, where it no longer views the ABZ. With two HEO satellites, continuous GEO‐like viewing is possible (aside from external factors like the available sunlight) with a number of different HEO options with periods typically in the range of 12–24 hr and apogee altitudes that are comparable to GEO (Trishchenko et al, ; Tritchtchenko et al, ).…”
Section: Highly Elliptical Orbits For Remote Sensing Of the Abz (Ray mentioning
confidence: 99%
“…By selecting the inclination of the orbit to situate the apogee near the critical inclination of 63.44°N, a single satellite can make quasi‐geostationary observations of the ABZ for a limited time before accelerating toward perigee, where it no longer views the ABZ. With two HEO satellites, continuous GEO‐like viewing is possible (aside from external factors like the available sunlight) with a number of different HEO options with periods typically in the range of 12–24 hr and apogee altitudes that are comparable to GEO (Trishchenko et al, ; Tritchtchenko et al, ).…”
Section: Highly Elliptical Orbits For Remote Sensing Of the Abz (Ray mentioning
confidence: 99%
“…We modeled it for all considered types of orbit with periods of #24 h using the European Space Agency (ESA) Space Environment Information System (SPENVIS) (Heynderickx et al 2004). The SPENVIS model setup follows that one presented in Trichtchenko et al (2014) and Trishchenko et al (2019) and is briefly summarized below. The radiation models for the trapped protons AP8 and electrons AE8 (Sawyer and Vette 1976;Vette 1991) have been utilized for conditions of a solar maximum for consistency with our previous analysis providing conservative estimates.…”
Section: Space Radiation Environmentmentioning
confidence: 99%
“…The total ionizing dose and its components have been estimated using SPENVIS built-in model ''SHIELDOSE'' (Seltzer 1980) with shielding configuration for the finite aluminum slab and the silicon (Si) as target material. The logarithmic values of ionizing dose have been interpolated to derive shielding thickness for an annual total ionizing dose (TID) value selected equal to 3.33 krad, which corresponds to accumulated TID equal to 50 krad for 15-yr space mission (Emmanuel et al 2014;Trichtchenko et al 2014;Trishchenko et al 2019).…”
Section: Space Radiation Environmentmentioning
confidence: 99%
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“…This is, e.g. the long-term SEU rate for a device with a 4 mm shield thickness on a highly elliptical orbit [29] as computed by European Space Agency's Space Environment Information System).…”
Section: Fault Scenariosmentioning
confidence: 99%