TY - GEN
T1 - Remote sensing of venusian seismic activity with a small spacecraft, the VAMOS mission concept
AU - DIdion, Alan
AU - Komjathy, Attila
AU - Sutin, Brian
AU - Nakazono, Barry
AU - Karp, Ashley
AU - Wallace, Mark
AU - Lantoine, Gregory
AU - Krishnamoorthy, Siddharth
AU - Rud, Mayer
AU - Cutts, James
AU - Lognonné, Philippe
AU - Kenda, Balthasar
AU - Drilleau, Mélanie
AU - Makela, Jonathan
AU - Grawe, Matthew
AU - Helbert, Jörn
N1 - Funding Information:
This material is based upon work supported by the National Aeronautics and Space Administration under ROSES 2016 NNH16ZDA001N-PSDS3 issued through the Planetary Science Deep Space SmallSat Studies Program. Support to the French team has been provided by CNES. This work was conducted at the NASA Jet Propulsion Laboratory, a division of California Institute of Technology.
Funding Information:
Jonathan Makela received the B.S. degree with honors in electrical engineering and the Ph.D. degree in electrical and computer engineering from Cornell University, Ithaca, NY, USA, in 1999 and 2003, respectively. From 2002–2004, he was a National Research Council Research Associate at the Naval Research Laboratory in Washington, DC, USA. He joined the faculty of the Department of Electrical and Computer Engineering at the University of Illinois at Urbana-Champaign, Urbana, IL, USA, as an Assistant Professor in 2004 and, since 2014, has held the rank of Professor. He is also a Research Professor in the Coordinated Science Laboratory at the University of Illinois at Urbana-Champaign. He is the (co-)author of more than 100 peer-reviewed articles. His research interests lie in multi-technique remote sensing of the Earth’s ionosphere and understanding the effects of space weather on critical technologies. Dr. Makela is a member of the American Geophysical Union, the International Union of Radio Science (URSI), Commission G, and the Committee on Space Research (COSPAR). He received the NSF CAREER award in 2007, the Zeldovich Medal from COSPAR and the Russian Academy of Sciences in 2008, the Henry G. Booker Fellowship from URSI in 2008, and the Mac Van Valkenburg Early Career Teaching Award from the IEEE Education Society in 2011. Siddharth Krishnamoorthy is a Postdoctoral Associate at the NASA Jet Propulsion Laboratory/California Institute of Technology and is working to develop technologies for remote seismology on Venus. Prior to joining JPL, he received his MS and PhD in aeronautics and astronautics from Stanford University, and a Masters degree in physics from the Indian Institute of Technology, Delhi. His current research interests are in the development of enabling technologies for planetary exploration systems, especially those related to remote sensing and entry, descent, and landing (EDL). Mayer Rud, Optical engineer and designer at NASA’s Jet Propulsion Laboratory, specializing in optical concept development, optical design, modeling and simulation. Mayer is the VAMOS Optical Engineer and Designer. Matthew Grawe received the B.S. degree with highest honors and the M.S. degree in electrical and computer engineering in from the University of Illinois, Urbana-Champaign, Urbana, IL USA, in 2015 and 2017, respectively. He is currently pursuing the Ph.D. degree at the University of Illinois at Urbana-Champaign. He was awarded 1st place prizes at the NSF-sponsored Coupling, Energetics, and Dynamics of Atmospheric Regions (CEDAR) workshops taking place in 2015 and 2017, respectively. His research interests lie in utilizing remote sensing techniques to understand geological and atmospheric phenomena Jörn Helbert is a physicist with a focus on planetary remote sensing and laboratory spectroscopy. Helbert is head of the “Planetary Spectroscopy Laboratories“ at DLR, coordinating the „Distributed Planetary Simulation Facility“ in the EuroPlanet Research infrastructure and member of a NASA SSERVI team. At DLR since 1998 he has served as participating scientist on the NASA MESSENGER mission as well as co-investigator on VenusExpress. Currently he is Co-I on ESA MarsExpress, JAXA Hayabusa 2 and the upcoming ESA ExoMars mission. He is Co-I of the MERTIS instrument on the ESA-JAXA BepiColombo mission to Mercury. Helbert received a diploma in Physics from the Technical University in Braunschweig, Germany and a doctorate in Natural Science from the Free University, Berlin, Germany. He is vice chair of the Union Commission on Planetary Science of the IUGG.
Publisher Copyright:
© 2018 IEEE.
PY - 2018/6/25
Y1 - 2018/6/25
N2 - The Venusian atmosphere creates inhospitable temperature and pressure conditions for the surface of Venus, Earth's twin planet, making in-situ measurements of any appreciable length difficult, expensive, and risky to obtain. Yet, because of the apparent youthfulness of Venus' surface features, long-duration seismic observations are in high demand in order to determine and understand the dynamic processes taking place in lieu of plate tectonics. The Venus Airglow Measurements and Orbiter for Seismicity (VAMOS) mission concept would make use of the dense Venusian atmosphere as a medium to conduct seismic vibrations from the surface to the ionosphere. Here, the resulting atmospheric gravity waves and acoustic waves can be observed in the form of perturbations in airglow emissions, the basic principles for which have been demonstrated at Earth following a tsunami and at Venus with the European Venus Express's Visible and Infrared Thermal Imaging Spectrometer (VIRTIS) instrument. In addition, these observations would enable VAMOS to determine the crustal structure and ionospheric variability of Venus without approaching the surface or atmosphere themselves. Equipped with an instrument of modest size and mass, the baseline VAMOS spacecraft is designed to fit within a SmallSat form factor and travel to Venus predominantly under its own power. VAMOS would enter into an orbit uniquely suited for the long-duration, full-disk staring observations required for seismic readings. VAMOS' journey would be enabled by modern solar electric propulsion technology and SmallSat avionics, which allow the spacecraft to reach Venus and autonomously filter observation data on board to detect Venus-quake events. Currently, trade studies are being conducted to determine mission architecture robustness to launch and rideshare opportunities. Key spacecraft challenges for VAMOS, just as with many SmallSat-based mission concepts, include thermal and power management, onboard processing capabilities, telecommunications throughput, and propulsion technology. The VAMOS mission concept is being studied at JPL as part of the NASA Planetary Science Deep Space SmallSat Studies (PSDS3) program, which will not only produce a viable and exciting mission concept for a Venus SmallSat, but will have the opportunity to examine many issues facing the development of SmallSats for planetary exploration. These include SmallSat solar electric propulsion, autonomy, telecommunications, and resource management that can be applied to various inner solar system mission architectures.
AB - The Venusian atmosphere creates inhospitable temperature and pressure conditions for the surface of Venus, Earth's twin planet, making in-situ measurements of any appreciable length difficult, expensive, and risky to obtain. Yet, because of the apparent youthfulness of Venus' surface features, long-duration seismic observations are in high demand in order to determine and understand the dynamic processes taking place in lieu of plate tectonics. The Venus Airglow Measurements and Orbiter for Seismicity (VAMOS) mission concept would make use of the dense Venusian atmosphere as a medium to conduct seismic vibrations from the surface to the ionosphere. Here, the resulting atmospheric gravity waves and acoustic waves can be observed in the form of perturbations in airglow emissions, the basic principles for which have been demonstrated at Earth following a tsunami and at Venus with the European Venus Express's Visible and Infrared Thermal Imaging Spectrometer (VIRTIS) instrument. In addition, these observations would enable VAMOS to determine the crustal structure and ionospheric variability of Venus without approaching the surface or atmosphere themselves. Equipped with an instrument of modest size and mass, the baseline VAMOS spacecraft is designed to fit within a SmallSat form factor and travel to Venus predominantly under its own power. VAMOS would enter into an orbit uniquely suited for the long-duration, full-disk staring observations required for seismic readings. VAMOS' journey would be enabled by modern solar electric propulsion technology and SmallSat avionics, which allow the spacecraft to reach Venus and autonomously filter observation data on board to detect Venus-quake events. Currently, trade studies are being conducted to determine mission architecture robustness to launch and rideshare opportunities. Key spacecraft challenges for VAMOS, just as with many SmallSat-based mission concepts, include thermal and power management, onboard processing capabilities, telecommunications throughput, and propulsion technology. The VAMOS mission concept is being studied at JPL as part of the NASA Planetary Science Deep Space SmallSat Studies (PSDS3) program, which will not only produce a viable and exciting mission concept for a Venus SmallSat, but will have the opportunity to examine many issues facing the development of SmallSats for planetary exploration. These include SmallSat solar electric propulsion, autonomy, telecommunications, and resource management that can be applied to various inner solar system mission architectures.
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U2 - 10.1109/AERO.2018.8396447
DO - 10.1109/AERO.2018.8396447
M3 - Conference contribution
AN - SCOPUS:85049837763
T3 - IEEE Aerospace Conference Proceedings
SP - 1
EP - 14
BT - 2018 IEEE Aerospace Conference, AERO 2018
PB - IEEE Computer Society
T2 - 2018 IEEE Aerospace Conference, AERO 2018
Y2 - 3 March 2018 through 10 March 2018
ER -