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2012
Authors: Bushman Stewart
Title: Design, Fabrication, and Testing of the Radiation Belt Storm Probes Propulsion Systems
Abstract: The Radiation Belt Storm Probes spacecraft , part of NASA’s Living with a Star program, are scheduled for launch into Earth orbit in August 2012. 1,2,3 The twin spacecraft possess identical blowdown monopropellant hydrazine propulsion systems to provide spinup/spindown, precession, Delt a–V, and deorbit capability. Each spacecraft manifests eight Aerojet 0.2 lbf (0.9 N) MR–103G thrust ers, three ARDÉ Inconel 718 propellant tanks, and other components required to control the fl ow of propellant and monitor system health and performance. The propulsion systems were fabricated and installed by Aerojet Redmond and subsequently tested at the Jo hns Hopkins University / Applied Physics Laboratory (APL) in Laurel, MD. The test se quence at APL included thermal balance; . . .
Date: 08/2012 Publisher: American Institute of Aeronautics and Astronautics DOI: 10.2514/6.2012-4332 Available at: http://arc.aiaa.org/doi/abs/10.2514/6.2012-4332
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Authors: Butler Michael, and Laughery Sean
Title: The RBSP Spacecraft Power System Design and Development
Abstract: The RBSP (Radiation Belt Storm Probes) twin spacecraft are set to launch in August 2012. The spacecraft will be inserted into the highly elliptical regions of high energy particles trapped by the magnetic field of the earth. These regions are often referred to as the Van Allen Belts. The twin spacecraft will operate entirely within the radiation belts throughout their mission. Because of the intense environment of operation and to reduce cost and risk, the approach taken in the power system electronics was to use quasi conventional design, materials, and fabrication techniques encased in a 350mil thick aluminum enclosure. The spacecraft are spin stabilized with an axial boom that creates a shadow across the solar arrays. The power system topology selected was a 28V unregulat. . .
Date: 08/2012 Publisher: American Institute of Aeronautics and Astronautics DOI: 10.2514/MIECEC1210.2514/6.2012-4059 Available at: http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4059
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Authors: Min Kyungguk, Lee Jeongwoo, Keika Kunihiro, and Li W
Title: Global distribution of EMIC waves derived from THEMIS observations
Abstract: [1] Electromagnetic ion cyclotron (EMIC) waves play an important role in magnetospheric dynamics and their global distribution has been of great interest. This paper presents the distribution of EMIC waves over a broader range than ever before, as enabled by observations with the Time History of Events and Macroscale Interactions during Substorms (THEMIS) spacecraft from 2007 to 2010. Our major findings are: (1) There are two major peaks in the EMIC wave occurrence probability. One is at dusk and 8–12 RE where the helium band dominates the hydrogen band waves. The other is at dawn and 10–12 RE where the hydrogen band dominates the helium band waves. (2) In terms of wave spectral power the dusk events are stronger (≈10 nT2/Hz) than the dawn events (≈3 nT2/Hz). (3) The dawn . . .
Date: 05/2012 Publisher: Journal of Geophysical Research DOI: 10.1029/2012JA017515
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Authors: Kirby Karen, Bushman Stewart, Butler Michael, Conde Rich, Fretz Kristen, et al.
Title: Radiation Belt Storm Probe Spacecraft and Impact of Environment on Spacecraft Design
Abstract: NASA's Radiation Belt Storm Probe (RBSP) is an Earth-orbiting mission scheduled to launch in September 2012 and is the next science mission in NASA's Living with a Star Program. The RBSP mission will investigate, characterize and understand the physical dynamics of the radiation belts, and the influence of the sun on the earth's environment, by measuring particles, electric and magnetic fields and waves that comprise the geospace. The mission is composed of two identically instrumented spinning spacecraft in an elliptical orbit around earth from 600 km perigee to 30,000 km apogee at 10 degree inclination to provide full sampling of the Van Allen radiation belts. The twin spacecraft will follow slightly different orbits and will lap each other 4 times per year; this offers simultaneous meas. . .
Date: 03/2012 Publisher: IEEE DOI: 10.1109/AERO.2012.6187020 Available at: http://ieeexplore.ieee.org/stamp/stamp.jsp?arnumber=06187020
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2011
Authors: Ukhorskiy Aleksandr Y., Mauk Barry H., Fox Nicola J., Sibeck David G., and Grebowsky Joseph M.
Title: Radiation belt storm probes: Resolving fundamental physics with practical consequences
Abstract: The fundamental processes that energize, transport, and cause the loss of charged particles operate throughout the universe at locations as diverse as magnetized planets, the solar wind, our Sun, and other stars. The same processes operate within our immediate environment, the Earth's radiation belts. The Radiation Belt Storm Probes (RBSP) mission will provide coordinated two-spacecraft observations to obtain understanding of these fundamental processes controlling the dynamic variability of the near-Earth radiation environment. In this paper we discuss some of the profound mysteries of the radiation belt physics that will be addressed by RBSP and briefly describe the mission and its goals.
Date: 07/2011 Publisher: Journal of Atmospheric and Solar-Terrestrial Physics Pages: 1417 - 1424 DOI: 10.1016/j.jastp.2010.12.005 Available at: http://www.sciencedirect.com/science/article/pii/S1364682610003688
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Authors: Millan R.M.
Title: Understanding relativistic electron losses with BARREL
Abstract: The primary scientific objective of the Balloon Array for RBSP Relativistic Electron Losses (BARREL) is to understand the processes responsible for scattering relativistic electrons into Earth's atmosphere. BARREL is the first Living with a Star Geospace Mission of Opportunity, and will consist of two Antarctic balloon campaigns conducted in the 2012 and 2013 Austral summer seasons. During each campaign, a total of 20 small View the MathML source(∼20kg) balloon payloads will be launched, providing multi-point measurements of electron precipitation in conjunction with in situ measurements from the two RBSP spacecraft, scheduled to launch in May 2012. In this paper we outline the scientific objectives of BARREL, highlighting a few key science questions that will be addressed by BARREL in c. . .
Date: 07/2011 Publisher: Journal of Atmospheric and Solar-Terrestrial Physics Pages: 1425 - 1434 DOI: 10.1016/j.jastp.2011.01.006 Available at: http://www.sciencedirect.com/science/article/pii/S1364682611000071
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2010
Authors: Min Kyungguk, Lee Jeongwoo, and Keika Kunihiro
Title: Chorus wave generation near the dawnside magnetopause due to drift shell splitting of substorm-injected electrons
Abstract: We study the relationship between the electron injection and the chorus waves during a substorm event on 23 March 2007. The chorus waves were detected at high geomagnetic latitude (∼70°S) Antarctic observatories in the range of 0600–0900 h in magnetic local time (MLT). Electrons drifting from the injection event were measured by two LANL spacecraft at 0300 and 0900 MLT. The mapping of auroral brightening areas to the magnetic equator shows that the injection occurred in an MLT range of 2200–2400. This estimate is consistent with observations by the THEMIS A, B, and D spacecraft (which were located at 2100 MLT and did not observe electron injections). Our backward model tracing from the magnetic equator near the dawnside magnetopause (which magnetically connects to the Antar. . .
Date: 10/2010 Publisher: American Geophysical Union DOI: 10.1029/2010JA015474
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2009
Authors: Kemp Brian L, McGee Timothy G, and Shankar Uday J
Title: Analysis of Spinning Spacecraft with Wire Booms Part 1: Derivation of Nonlinear Dynamics
Abstract: Algebraic expressions for the governing equations of motion are developed to describe a spinning spacecraft with flexible appendages. Two limiting cases are investigated: appendages that are self-restoring and appendages that require spacecraft motion to restore. Solar panels have sufficient root stiffness to self-restore perturbations. Radial wire antennae have little intrinsic root stiffness and require centripetal acceleration from spacecraft rotations to restore perturbations. External forces applied for attitude corrections can displace spacecraft appendages from their steady-state position. The Radiation Belt Storm Probe (RBSP) satellite is used as an example to explore numerical results for several maneuvers.
Date: 08/2009 Publisher: AIAA Guidance, Navigation, and Control Conference DOI: 10.2514/6.2009-6202 Available at: http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6202
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Authors: McGee Timothy G, Shankar Uday J, and Kemp Brian L
Title: Analysis of Spinning Spacecraft with Wire Booms Part 2: Out-of-Plane Dynamics and Maneuvers
Abstract: An analysis of the dynamics for a spin stabilized spacecraft consisting of a rigid central hub with four long exible wire booms is presented. The analysis focuses on the dynamics out of the spin plane of the spacecraft. Companion papers will focus on the derivations of the full nonlinear dynamics and analysis of the in plane dynamics. A linear analysis is used to estimate the mode shapes of the free response of the system, the e ects of various damping mechanisms on these modes, and the dynamic response of the system to various maneuvers. The results of an independent simulation of the full nonlinear dynamics of the system are also provided to support the linear analysis. While the dynamics and analysis approach presented can be applied to the general class of spin stabilized space. . .
Date: 08/2009 Publisher: AIAA Guidance, Navigation, and Control Conference DOI: 10.2514/6.2009-6203 Available at: http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6203
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Authors: Shankar Uday J, McGee Timothy G, and Kemp Brian L
Title: Analysis of Spinning Spacecraft with Wire Booms Part 3: Spin-Plane Dynamics, Maneuvers, and Deployment
Abstract: Several science spacecraft use long wire booms as electric-field antennas and the spacecraft spins to maintain the orientation of these flexible wires. These booms account for a majority of the total spacecraft inertia while weighing only a small fraction of the total mass. The spacecraft dynamics is therefore dominated by these booms. The analysis of such spacecraft is further complicated by other flexible ap- pendages and the presence of damping in the system, both inherent in the sys- tem and from damping mechanisms deliberately added into the system. This pa- per and two companion papers analyze such spacecraft. The first of these derives the governing nonlinear equations from first principles. Under certain conditions, the dynamics neatly separate into spin-plane and out-of-p. . .
Date: 08/2009 Publisher: AIAA Guidance, Navigation, and Control Conference DOI: 10.2514/6.2009-6204 Available at: http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6204
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2007
Authors: Reeves Geoffrey D
Title: Radiation Belt Storm Probes: The Next Generation of Space Weather Forecasting
Abstract: N/A
Date: 11/2007 Publisher: Space Weather DOI: 10.1029/2007SW000341 Available at: http://www.agu.org/pubs/crossref/2007/2007SW000341.shtml
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