2009
DOI: 10.1007/s11214-009-9504-y
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The Interstellar Boundary Explorer High Energy (IBEX-Hi) Neutral Atom Imager

Abstract: The IBEX-Hi Neutral Atom Imager of the Interstellar Boundary Explorer (IBEX) mission is designed to measure energetic neutral atoms (ENAs) originating from the interaction region between the heliosphere and the local interstellar medium (LISM). These ENAs are plasma ions that have been heated in the interaction region and neutralized by charge exchange with the cold neutral atoms of the LISM that freely flow through the interaction region. IBEX-Hi is a single pixel ENA imager that covers the ENA spectral range… Show more

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Cited by 191 publications
(122 citation statements)
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“…It features two singlepixel, neutral atom cameras: IBEX-Hi (Funsten et al 2009) and IBEX-Lo (Fuselier et al 2009). Basically only IBEX-Lo has the capability of discerning species of the incoming atoms, including (indirectly) neutral He (Möbius et al 2009), and IBEX-Hi was designed to observe neutral H. Allegrini et al (2008) suggest an ingeneous technique by which some other species, including He, might also be registered owing to a special treatment of data from the IBEX-Hi anti-coincidence system.…”
Section: Final Discussion and Conclusionmentioning
confidence: 99%
“…It features two singlepixel, neutral atom cameras: IBEX-Hi (Funsten et al 2009) and IBEX-Lo (Fuselier et al 2009). Basically only IBEX-Lo has the capability of discerning species of the incoming atoms, including (indirectly) neutral He (Möbius et al 2009), and IBEX-Hi was designed to observe neutral H. Allegrini et al (2008) suggest an ingeneous technique by which some other species, including He, might also be registered owing to a special treatment of data from the IBEX-Hi anti-coincidence system.…”
Section: Final Discussion and Conclusionmentioning
confidence: 99%
“…Since the spectra are measured in the spacecraft frame, we transform the model distributions, Equations (1) and (2), from the solar wind frame into the spacecraft frame using a non-relativistic velocity transformation, v + u = v c + v m , where v c is the velocity of the spacecraft relative to the Sun, and u is the solar wind bulk velocity, which we assume to be constant and in the radial direction for this analysis. An instrument's geometric factor, G, is defined by an integration of the response function R(v m ; V ) over v m and is related proportionally to the measured count rate (Funsten et al 2009;Johnstone et al 1987;Hundhausen et al 1967). Typically for ESA-based instruments, the geometric factor, G, is assumed to be independent of E/q.…”
Section: Discussionmentioning
confidence: 99%
“…McNutt et al (1999) already provided the proton-hydrogen chargeexchange cross section in the power law form σ (ε) ∼ = σ 0 · ε −b cs , with σ 0 ≈ 2.4280 × 10 −15 cm 2 and b cs ≈ 0.1327, which is valid over an energy range that includes the IBEX-Hi energy channels #2-6 with range 0.71-4.29 keV (Funsten et al 2009b). (Throughout this work, energy will be given in keV.)…”
Section: Theorymentioning
confidence: 99%