Low-altitude Spacecraft Research Articles

Latituditual Structure of Dayside Polar Cusp Precipitation

The results of observations of low-altitude spacecraft crossing the daytime sector of the auroral zone and of high-apogee spacecraft in the equatorial plane of the magnetosphere were analyzed in order to identify the main processes leading to the formation of dayside polar cusps. Observations from the DMSP F7 spacecraft were used to analyze the latitudinal characteristics of ion precipitation in the cusp region and to study the latitudinal profile of ion pressure in the cusp depending on the IMF parameters. A significant difference was found in identifying the cusp boundaries using an automated data processing system and direct analysis of spacecraft observations. It is shown that for small negative values of the Bz-component of the IMF (〈Bz〉 = –3.0 nT), an ordinary feature of the cusp is the latitudinal profile of the ion pressure (Pi) with a width of ~1° of latitude with two maxima, one of which is located in the equatorward and the other in the poleward of the cusp. For large negative Bz values (–6, –8 nT), the polar maximum in the latitudinal profile Pi disappears; only the equatorial maximum remains, the Pi level at the maximum increases, and the width of the cusp decreases to ~0.7°. For Bz IMF 0, the most characteristic is the Pi profile with a maximum ion pressure in the polar part of the cusp. The cusp for Bz 0 is located at higher latitudes than for Bz 0, and its average latitudinal width increase to ~1.4° of latitude. In the prenoon sector MLT, the most typical for periods with a large negative By-component of the IMF (〈By〉 = –6.3 nT, 〈Bz〉 = –1.7 nT) is a cusp with a width of ~1.4° of latitude with a flat top in the latitudinal Pi profile. Comparison of the pressure distributions observed at low heights with data from high-apogee satellites confirmed the possibility of describing the formation of the cusp as a diamagnetic cavity and using observations in the cusp to determine the ion pressure in the magnetosheath.

Lifetime Extension of Ultra Low-Altitude Lunar Spacecraft with Low-Thrust Propulsion System

Due to the non-spherical perturbation of the Moon, the lifetime of ultra low-altitude Lunar spacecraft may be quite short. In this paper, we analyze the lifetime of about 50 km-altitude Lunar spacecraft with different initial orbit. The lifetime in low inclination orbits is much shorter than the ones in the near polar orbits. To extend the lifetime and keep the spacecraft in an appropriate range, an orbit maintenance strategy based on low-thrust propulsion system is proposed. The influence of the orbit initial conditions (e.g., semi-major axis, inclination, right ascension of the ascending node) on lifetime extension are discussed and the effect of the low-thrust magnitude in orbit maintenance is analyzed. According to the numerical simulation results, the lifetime of about 50 km-altitude 100 kg Lunar spacecraft with 10 kg fuel and 20 mN thruster can be extended from 7.958 days to over a 109.1725 days, which demonstrates the effectiveness of the strategy. Furthermore, a global perspective for ultra low-altitude Lunar spacecraft lifetime extension problem is provided in this paper, which can be applied to Moon mission designs extensively.

A Review of Cluster Wideband Data Multi‐Spacecraft Observations of Auroral Kilometric Radiation

AbstractWe review important advances in the understanding of auroral kilometric radiation (AKR) resulting from observations by the Wideband Data instruments on the four Cluster spacecraft. AKR is an intense radio emission originating in the Earth's auroral regions with frequencies typically in the range 50–700 kHz, usually observed from space. It is now widely accepted that AKR is generated by the cyclotron maser instability (CMI) in density cavities in the auroral acceleration region. Multi‐point observations by the Cluster spacecraft with a time delay of arrival technique have allowed the source locations of many individual AKR bursts to be determined. The position uncertainty is around 500 km at the source region or about 200 km when mapped on to the auroral zone. AKR is emitted in a narrow beam close to the tangent to the magnetic field vector in the source region. This has important implications for the possible generation mechanisms, being incompatible with filled or hollow cone beaming models. It also implies that an observer at a given location can only see AKR from a fraction of possibly active source regions. The complex frequency time structure of AKR sometimes shows regular striations or pulsations. Cluster observations of these phenomena have been interpreted as modulation of the CMI by disturbances propagating through the generation region. Exceptionally, AKR can sometimes be observed from low altitude spacecraft or even on the ground. Recent work has involved simultaneous observations of AKR on the Cluster spacecraft and on the ground at the South Pole.

Charged particle scattering in dipolarized magnetotail

The Earth's magnetotail is characterized by stretched magnetic field lines. Energetic particles are effectively scattered due to the field-line curvature, which then leads to isotropization of energetic particle distributions and particle precipitation to the Earth's atmosphere. Measurements of these precipitation at low-altitude spacecraft are thus often used to remotely probe the magnetotail current sheet configuration. This configuration may include spatially localized maxima of the curvature radius at equator (due to localized humps of the equatorial magnetic field magnitude) that reduce the energetic particle scattering and precipitation. Therefore, the measured precipitation patterns are related to the spatial distribution of the equatorial curvature radius that is determined by the magnetotail current sheet configuration. In this study, we show that, contrary to previous thoughts, the magnetic field line configuration with the localized curvature radius maximum can actually enhance the scattering and subsequent precipitation. The spatially localized magnetic field dipolarization (magnetic field humps) can significantly curve magnetic field lines far from the equator and create off-equatorial minima in the curvature radius. Scattering of energetic particles in these off-equatorial regions alters the scattering (and precipitation) patterns, which has not been studied yet. We discuss our results in the context of remote-sensing the magnetotail current sheet configuration with low-altitude spacecraft measurements.

Variations in Energetic Particle Fluxes around Significant Geomagnetic Storms Observed by the Low-Altitude DEMETER Spacecraft

A superposed epoch analysis is conducted for five geomagnetic storms in the years 2005 and 2006 with the aim to understand energetic particle flux variations as a function of L-shell, energy and time from the Dst minimum. Data measured by the low-altitude DEMETER spacecraft were used for this purpose. The storms were identified by a Dst index below −100 nT, as well as their being isolated events in a seven-day time window. It is shown that they can be categorized into two types. The first type shows significant variations in the energetic particle fluxes around the Dst minimum and increased fluxes at high energies (>1.5 MeV), while the second type only shows increased fluxes around the Dst minimum without the increased fluxes at high energies. The first type of storm is related to more drastic but shorter-lasting changes in the solar wind parameters than the second type. One storm does not fit either category, exhibiting features from both storm types. Additionally, we investigate whether the impenetrable barrier for ultra-relativistic electrons also holds in extreme geomagnetic conditions. For the highest analyzed energies, the obtained barrier L-shells do not go below 2.6, consistent with previous findings.

Ion Pressure in Different Regions of the Dayside Auroral Precipitation

The ion pressure in the regions of ionospheric projections of the plasma mantle, polar cusp, low-latitude boundary layer, and the region of structured precipitation of the auroral oval during magnetic calm is studied based on data from the DMSP F6 and F7 low-altitude spacecraft. It is shown that the level of ion pressure in all of these regions does not depend on either the polarity or the value of the Bz component of the IMF. The ion pressure in the mantle varies from 0.02 to 0.06 nPa and does not depend on the magnitude of the solar wind dynamic pressure. The average pressure level is $$\left\langle {Pm} \right\rangle $$ = 0.03 ± 0.01 nPa. In the cusp area at IMF Bz > 0, the ion pressure (Pc) does not depend on the solar wind dynamic pressure (Psw), while the pressure at IMF Bz < 0 increases significantly with the increasing in Psw. The average pressure level is $$\left\langle {Pc} \right\rangle $$ = 1.0 ± 0.3 nPa, which is almost two orders of magnitude higher than that in the mantle. The ion pressure also increases with the solar wind dynamic pressure in both the LLBL and the auroral oval precipitation (AOP). The average pressure in the LLBL is $$\left\langle {{{P}_{L}}} \right\rangle $$ = 0.27 ± 0.07 nPa, while in the AOP region its average value is two times lower. The MLT pressure pattern in LLBL shows a pronounced increase in the noon sector (~11–14 MLT), the value of which increases with increasing in the solar wind dynamic pressure. In the AOP region the pressure is distributed over MLT fairly evenly, which results in a significant pressure difference (ΔP = PL – PA) in the noon sector between the low-latitude boundary layer and the auroral oval.

Impact of Earth’s Magnetic Field Secular Drift on the Low-Altitude Proton Radiation Belt From 1900 to 2050

The effects of the space radiation environment on spacecraft systems and instruments are significant design considerations for space missions. In order to meet these challenges and have reliable, cost-effective designs, the radiation environment must be understood and accurately modeled. The low-altitude proton environment varies slowly in time due to the secular drift of Earth’s main magnetic field and due to the evolution of the solar cycle. The purpose of this paper is to extend the onera proton altitude low model capabilities by introducing a prediction of Earth’s main magnetic field model up to the year 2050. Impact on low-altitude spacecraft radiation specification for next space missions is then assessed.

The Technology of LEO Satellite Communication Systems Utilization for the Rapid Exchange of Data with the Low-altitude Spacecraft: Scientific Technological Equipment “Kontakt-MKA” On the Small Spacecraft “AIST-2”

In this paper was analyzed thepossibility ofcommunication sessions withthe small spacecraftvia theGlobalstarsystem. Theduration of communicationsessions was estimated.It was made astochasticanalysis ofthe data transmission capabilitiesbetween the twospacecraftvia theGlobalstarsystem. The probability ofdata transmission between twospacecraft, depending on data volumeandworkload ofthe Globalstar system was estimated. The spaceexperiment on thesmall spacecraft “AIST-2” is planning to testthe results.

Closed-Form Approximation of Revisit Rate for Low-Altitude Satellites

For many applications of low-altitude spacecraft, it is important to know how often the spacecraft revisits a given target. Average revisits per day can be calculated for a given scenario using astrodynamic software, but that approach can be tedious if a large number of cases are to be compared. This paper develops a closed-form, continuous, and piecewise differentiable function that gives average revisits per day as a function of orbit altitude, orbit inclination, target latitude, and minimum required elevation. The function is compared with the results of astrodynamic simulations and shown to be accurate to within 0.08 passes per day and 1% in almost all cases. It allows instant calculation of an excellent approximation of this important performance parameter and could be used as part of an optimization routine. The convenience and flexibility provided by this function are demonstrated in a series of charts showing passes per day as a function of one, two, and three variables. The function assumes a circular orbit; the sensitivity of the result to eccentricity is explored using astrodynamic simulations and is found to decrease by 5.3% as eccentricity increases to 0.07 for a typical case.

Focusing on Size and Energy Dependence of Electron Microbursts From the Van Allen Radiation Belts

Focusing on Size and Energy Dependence of Electron Microbursts From the Van Allen Radiation Belts

Magnetic field direction and lunar swirl morphology: Insights from Airy and Reiner Gamma

Many of the Moon's crustal magnetic anomalies are accompanied by high albedo features known as swirls. A leading hypothesis suggests that swirls are formed where crustal magnetic anomalies, acting as mini magnetospheres, shield portions of the surface from the darkening effects of solar wind ion bombardment, thereby leaving patches that appear bright compared with their surroundings. If this hypothesis is correct, then magnetic field direction should influence swirl morphology. Using Lunar Prospector magnetometer data and Clementine reflectance mosaics, we find evidence that bright regions correspond with dominantly horizontal magnetic fields at Reiner Gamma and that vertical magnetic fields are associated with the intraswirl dark lane at Airy. We use a genetic search algorithm to model the distributions of magnetic source material at both anomalies, and we show that source models constrained by the observed albedo pattern (i.e., strongly horizontal surface fields in bright areas, vertical surface fields in dark lanes) produce fields that are consistent with the Lunar Prospector magnetometer measurements. These findings support the solar wind deflection hypothesis and may help to explain not only the general form of swirls, but also the finer aspects of their morphology. Our source models may also be used to make quantitative predictions of the near surface magnetic field, which must ultimately be tested with very low altitude spacecraft measurements. If our predictions are correct, our models could have implications for the structure of the underlying magnetic material and the nature of the magnetizing field.

우주 방사능에 의한 실리콘 태양 전지의 특성 변화

우주 방사선은 인공위성의 오동작을 유발하거나 수명을 단축하는 주된 요인 중 하나다. 반 알렌벨트라고 불리는 전하를 띤 고에너지 입자들이 지구 자기장에 포획된 공간은 이 지역에서 운용되는 인공위성뿐만 아니라, 지구 자기장을 따라 저고도까지 도달하므로 저궤도 위성들에게도 위협이 된다. 2003년 발사된 과학기술위성 1호에는 자세 제어를 위해 사용된 태양 센서가 탑재되었다. 태양 센서에는 빛을 감지하기 위한 검출기로 실리콘 태양 전지가 사용되었는데, 이 태양 전지의 합선 전류가 시간이 지남에 따라 감소하는 것이 관측되었다. 이 연구에서는 이러한 태양전지의 특성 변화가 어떠한 요인에 의해 발생하는지 지상에서의 방사능 실험을 통해 밝히고자 한다. 이를 위해 과학기술위성 1호에서 사용된 것과 동일한 태양 전지에 여러 에너지 대역의 고에너지 전자와 양성자를 조사하고 이 때 변하는 합선 전류를 측정하였다. 그리고 NOAA POES위성 데이터를 이용하여 과학기술위성 1호에 피폭되었을 방사선량을 예측하였다. 연구 결과, 과학기술위성 1호에 나타난 실리콘 태양 전지의 감쇠 현상은 700keV에서 1.5MeV의 에너지를 갖는 양성자에 의한 것으로 밝혀졌다. 이 연구 결과는 우주에서 태양 전지의 수명을 예측하기 위한 자료로 활용될 수 있다. High energy charged particles are trapped by geomagnetic field in the region named Van Allen Belt. These particles can move to low altitude along magnetic field and threaten even low altitude spacecraft. Space Radiation can cause equipment failures and on occasions can even destroy operations of satellites in orbit. Sun sensors aboard Science and Technology Satellite (STSAT-l) was designed to detect sun light with silicon solar cells which performance was degraded during satellite operation. In this study, we try to identify which particle contribute to the solar cell degradation with ground based radiation facilities. We measured the short circuit current after bombarding electrons and protons on the solar cells same as STSAT-1 sun sensors. Also we estimated particle flux on the STSAT-l orbit with analyzing NOAA POES particle data. Our result clearly shows STSAT-l solar cell degradation was caused by energetic protons which energy is about 700keV to 1.5MeV. Our result can be applied to estimate solar cell conditions of other satellites.

Multi-instrument mapping of the small-scale flow dynamics related to a cusp auroral transient

Abstract. In this paper we focus on flux transfer events (FTEs) and poleward moving auroral forms (PMAFs) in the cusp region, combining data from the EISCAT Svalbard radar, SuperDARN HF radars, ground-based optics, and three low-altitude polar-orbiting spacecraft. During an interval of southward interplanetary magnetic field the EISCAT Svalbard radar tracked a train of narrow flow channels drifting into the polar cap. One 30-60 km wide flow channel surrounded by flow running in the opposite direction is studied in great detail from when it formed equatorward of the cusp aurora, near magnetic noon, until it left the field-of-view and disappeared into the polar cap. Satellite data shows that the flow channel was on open field lines. The flow pattern is consistent with field-aligned currents on the sides of the flow channel; with a downward current on the equatorward side, and an upward current on the poleward side. The poleward edge of the flow channel was coincident with a PMAF that separated from the background cusp aurora and drifted into the polar cap. A passage of the DMSP F13 spacecraft confirms that the FTE flow channel was still discernable over 15 minutes after it formed, as the spacecraft revealed a 30–40 km wide region of sunward flow within the anti-sunward background convection. From the dimensions of the flow channel we estimate that the magnetic flux contained in the event was at least 1 MWb. This data set also shows that Birkeland current filaments often seen by low-altitude spacecraft in the cusp/mantle are really associated with individual FTE events or a train of FTEs in progress. As the region 0 or cusp/mantle current represents the statistical average consistent with the large-scale flow pattern, we therefore introduce a new term – FTE currents – to denote the unique pair of Birkeland current sheets that are associated with individual meso-scale FTE flow disturbances. The poleward moving auroral forms (PMAFs), often referred to in the literature, are the optical signature of the upward FTE current. Keywords. Magnetospheric physics (Current systems; Magnetopause, cusp and boundary layers) – Ionosphere (plasma convection)

The spherical segmented Langmuir probe in a flowing thermal plasma: numerical model of the current collection

Abstract. The segmented Langmuir probe (SLP) has been recently proposed by one of the authors (Lebreton, 2002) as an instrument to derive the bulk velocity of terrestrial or planetary plasmas, in addition to the electron density and temperature that are routinely measured by Langmuir probes. It is part of the scientific payload on the DEMETER micro-satellite developed by CNES. The basic concept of this probe is to measure the current distribution over the surface using independent collectors under the form of small spherical caps and to use the angular anisotropy of these currents to obtain the plasma bulk velocity in the probe reference frame. In order to determine the SLP capabilities, we have developed a numerical PIC (Particles In Cell) model which provides a tool to compute the distribution of the current collected by a spherical probe. Our model is based on the simultaneous determination of the charge densities in the probe sheath and on the probe surface, from which the potential distribution in the sheath region can be obtained. This method is well adapted to the SLP problem and has some advantages since it provides a natural control of the charge neutrality inside the simulation box, allows independent mesh sizes in the sheath and on the probe surface, and can be applied to complex surfaces. We present in this paper initial results obtained for plasma conditions corresponding to a Debye length equal to the probe radius. These plasma conditions are observed along the Demeter orbit. The model results are found to be in very good agreement with those published by Laframboise (1966) for a spherical probe in a thermal non-flowing plasma. This demonstrates the adequacy of the computation method and of the adjustable numerical parameters (size of the numerical box and mesh, time step, number of macro-particles, etc.) for the considered plasma-probe configuration. We also present the results obtained in the case of plasma flowing with mesothermal conditions reproducing the case of measurements onboard a low altitude spacecraft. Finally, we briefly discuss the capabilities of the SLP to deduce the plasma bulk velocity under similar conditions and present the first onboard measurements. Keywords. Ionosphere (Modeling and forecasting; Instruments and techniques)

&amp;lt;i&amp;gt;Letter to the Editor&amp;lt;/i&amp;gt;A statistical study of the location and motion of the HF radar cusp

Abstract. The large-scale and continuous monitoring of the ionospheric cusp region offered by HF radars has been exploited in order to examine the statistical location and motion of the equatorward edge of the HF radar cusp as a function of the upstream IMF BZ component. Although a considerable scatter is seen, both parameters have a clear influence from the north-south component of the IMF. Excellent agreement is achieved with previous observations from low altitude spacecraft data. The HF radar cusp region is seen to migrate equatorward at a rate of 0.02° min-1 nT-1 under IMF BZ south conditions, but remains static for IMF BZ north. The motion of the cusp implies an addition of magnetic flux of ~ 2 × 104 Wbs-1 nT-1 under IMF BZ south conditions, equivalent to a reconnection voltage of 20 kV nT-1, which is consistent with previous estimates from case studies on both the dayside and nightside regions.Key words. Ionosphere (auroral ionosphere) – Magnetospheric physics (magnetosphere-ionosphere interaction; solar wind magnetosphere interactions)

On the remote sensing of plasma sheet from low-altitude spacecraft

The possibility to estimate plasma sheet parameters from low-altitude measurements looks quite attractive, but it critically depends on how isotropic the plasma pressure is in the flux tube. To evaluate the ion pressure anisotropy we compare the values of pressure in the ionospheric and equatorial parts of the field line. Ionospheric values were computed from proton measurements at NOAA low-altitude satellites, they were compared with pressure estimates computed from empirical magnetic field models as well as with average values known from direct plasma sheet measurements. Three different methods of mapping the plasma pressure from plasma sheet to low altitude have been tried; each uses the particle isotropic boundaries observed at low altitudes and/or computed from magnetospheric models. Excluding observations obtained during substorm expansion, from these comparisons we conclude that in the plasma sheet, at geocentric distances 9–20 R E, the pressure estimates in the ionospheric and equatorial parts of the plasma sheet flux tube agree very well, suggesting a good pressure isotropy and thus justifying a possibility to monitor the plasma sheet parameters based on low-altitude measurements. The results also illustrate the usefulness of isotropic boundaries as a label of tail current intensity and as reliable tool for establishing mapping between magnetosphere and ionosphere.

Atmospheric Reentry Disposal for Low-Altitude Spacecraft

Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.

Remotely imaging the plasma sheet with low-altitude satellite clusters

Low-altitude satellites make latitudinal cuts through the entire plasma sheet within a few minutes. We show that by combining several such satellites it is possible to form an image of a large portion of the plasma sheet within a relatively short time. Strictly speaking such a technique images the field-aligned portion of the plasma sheet, however, theoretical work as well as extensive in situ observations have demonstrated that the plasma sheet is highly isotropic. In practice the most significant limitation is that electron acceleration events (including the auroral bulge) require discarding the associated ion data. An instance when five DMSP satellites (F10–F14) went through the southern hemisphere nightside oval within a 19 min period is used to construct the first partial magnetotail image. The possibilities of combining data from other missions to construct more complete composite images is considered. This technique is also highly useful in statistical studies of the plasma sheet. Because a low-altitude spacecraft cuts through the plasma sheet about 25 times as often as a mid-altitude spacecraft, and hundreds of times more often than high-altitude spacecraft, statistically meaningful surveys of the plasma sheet as a whole are hundreds of times easier using a collection of DMSP satellites. We demonstrate herein that the dawn LLBL flank is an apparent source of cold magnetosheath plasma supplied to the central plasma sheet.

Energetic neutral atom imaging of magnetospheric ions from high- and low-altitude spacecraft

We present a mapping from the 2-dimensional images formed by energetic neutral atoms (ENAs) to the phase space of physically relevant parameters of the energetic ion distributions that generate the images. This mapping of the lines of sight (LOS) for each image pixel into the L-MLT plane reveals the manner in which the LOS probe the spatial volume of the ion distribution as well as the configuration of its boundaries. Thus this mapping has direct application to the unfolding of ENA images obtained from both high- and low-altitude spacecraft.

Computer simulations of energetic neutral atom imaging from low and high altitude spacecraft

ENA cameras are being readied for flight on the Argentine SAC-B low-altitude mission and the NASA Cassini Saturn orbiter and an upcoming NASA MidEx mission (IMAGE) will be devoted completely to magnetospheric imaging. Computer simulation of ENA images has proved an indispensable tool for both scientific data analysis and instrument/mission design for a number of reasons. ENA emission is usually “optically thin”, so it is very difficult to imagine how magnetospheric ion distributions will image from different vantage points. ENA emission has a wide dynamic range in intensity, and contemporary cameras do not always have angular resolution sufficient to resolve the structures. Consequently, image simulation is an essential element in the extraction of the ion distributions from ENA images. Examples of simulations from past, present, and future missions that illustrate these effects are presented.