2009
DOI: 10.1007/s11214-009-9514-9
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The IBEX Flight Segment

Abstract: IBEX provides the observations needed for detailed modeling and in-depth understanding of the interstellar interaction (McComas et al. in

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Cited by 13 publications
(9 citation statements)
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“…The reason for the differences between the select ISM flow observation times and ES beam parameters is that because the spin axis of the spacecraft, which is never aligned with the Sun, does not change during an orbit (Scherrer et al 2009;H lond et al 2012), the beam of the NISHe gas, which in the solar inertial frame is invariant relative to the distant stars, wanders through the FOV of the sensor, changing gradually its angular size, peak location, and height. This effect is especially visible in the orbits before or after orbits 16 and 64 and is illustrated in lines, which, when averaged, would equal the thick blue lines.…”
Section: Collimator-averaged Signal As Function Of Spin Phasementioning
confidence: 99%
“…The reason for the differences between the select ISM flow observation times and ES beam parameters is that because the spin axis of the spacecraft, which is never aligned with the Sun, does not change during an orbit (Scherrer et al 2009;H lond et al 2012), the beam of the NISHe gas, which in the solar inertial frame is invariant relative to the distant stars, wanders through the FOV of the sensor, changing gradually its angular size, peak location, and height. This effect is especially visible in the orbits before or after orbits 16 and 64 and is illustrated in lines, which, when averaged, would equal the thick blue lines.…”
Section: Collimator-averaged Signal As Function Of Spin Phasementioning
confidence: 99%
“…The orientation of the Z-axis is periodically changed to approximately follow the Sun. Originally, the orientation of the spin-axis was modified after the perigee in each orbit (Scherrer et al 2009). After orbit 127 in 2011 June, IBEX was placed into a long-term stable lunar-resonance orbit (McComas et al 2011) and since then the IBEX spin-axis has been re-oriented twice per orbit, near apogee and perigee.…”
Section: Strategy Of Isn Observations By Ibexmentioning
confidence: 99%
“…Space Mission Capabilities (15) First use of additional Solid Rocket Motor on Pegasus LV and spacecraft propulsion to achieve very high altitude orbit. McComas et al 2009a;Scherrer et al 2009 (16) Discovery and first use of long-term stable lunar synchronous orbit.…”
Section: Mccomas Et Al 2009bmentioning
confidence: 99%
“…The Interstellar Boundary Explorer (IBEX) is the first, and thus far only, mission dedicated to imaging and understanding the interaction of our heliosphere with the local interstellar medium (LISM; see McComas et al 2009a and other papers in the IBEX Special Issue of Space Science Reviews). IBEX was launched on 2008 October 19, and after roughly two months of orbit raising to place it into its initial highly elliptical orbit (apogee ∼50 Earth radii; McComas et al 2009a;Scherrer et al 2009), began returning the first global observations of this interaction through measurements of energetic neutral atoms (ENAs).…”
Section: Introductionmentioning
confidence: 99%