{"id":944,"date":"2019-05-09T17:11:47","date_gmt":"2019-05-09T17:11:47","guid":{"rendered":"http:\/\/ippw2019.uk\/?page_id=944"},"modified":"2019-05-09T17:11:47","modified_gmt":"2019-05-09T17:11:47","slug":"poster-session-i","status":"publish","type":"page","link":"https:\/\/ippw2019.uk\/index.php\/poster-session-i\/","title":{"rendered":"Poster Session I"},"content":{"rendered":"
\n

Poster Session I - Tuesday 9th July 2019<\/h2>\n\n\n\n\n\t\n\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t\n\t
Order<\/th>1-min
\nOrder<\/th>		1-min Presentation before what session<\/th>Part of Which Session<\/th>Title<\/th>Name<\/th>Affiliation<\/th>Status<\/th>\n<\/tr>\n<\/thead>\n
A1
\n<\/td>		I.1.<\/td>Science Instrumentation, Experiments,
\nand In-Situ Measurements<\/td>		Science Instrumentation, Experiments, and In-
\nSitu Measurements<\/td>		INES-a flexible and innovative payload for measuring radiation in the presence of
\nablation<\/td>		Gilles BAILET<\/td>CentraleSup\u00e9lec<\/td><\/td>\n<\/tr>\n
A2<\/td>I.2<\/td>Science Instrumentation, Experiments,
\nand In-Situ Measurements<\/td>		Science Instrumentation, Experiments, and In-
\nSitu Measurements<\/td>		Laboratory-Based Thermal Shock Investigation of Heat Flux Sensors for the Mars 2020 Backshell<\/td>Ruth Miller<\/td>AMA Inc. at NASA Ames Research Center<\/td><\/td>\n<\/tr>\n
A3<\/td>I.3<\/td>Science Instrumentation, Experiments,
\nand In-Situ Measurements<\/td>		Science Instrumentation, Experiments, and In-
\nSitu Measurements<\/td>		The LONSCAPE (Light Optical Nephelometer Sizer and Counter for Aero-sols in Planetary Environments) instrument: concept and application for the in situ detection of liquid and solid particles<\/td>Jean-Baptiste Renard<\/td>LPC2E-CNRS<\/td><\/td>\n<\/tr>\n
A4<\/td>I.4<\/td>Science Instrumentation, Experiments,
\nand In-Situ Measurements<\/td>		Science Instrumentation, Experiments, and In-
\nSitu Measurements<\/td>		GeMini Plus: Preparing the Way for Future Planetary Elemental Composition
\nMeasurements Throughout the Solar System Using Gamma-Ray Spectroscopy<\/td>		John Goldsten<\/td>Johns Hopkins Applied Physics Laboratory<\/td><\/td>\n<\/tr>\n
A5<\/td>I.5<\/td>Science Instrumentation, Experiments,
\nand In-Situ Measurements<\/td>		Science Instrumentation, Experiments, and In-
\nSitu Measurements<\/td>		High Temperature Operation of Gallium Nitride Hall-Effect Sensors<\/td>Hannah Alpert<\/td>Stanford University<\/td>Student<\/td>\n<\/tr>\n
A6<\/td>I.6<\/td>Science Instrumentation, Experiments,
\nand In-Situ Measurements<\/td>		Science Instrumentation, Experiments, and In-
\nSitu Measurements<\/td>		An Energetic Particle Monitor for Ice Giant Atmospheric Probes<\/td>Nicolas Andre<\/td>IRAP, CNRS, UPS, CNES<\/td><\/td>\n<\/tr>\n
A7<\/td>I.7<\/td>Science Instrumentation, Experiments,
\nand In-Situ Measurements<\/td>		Science Instrumentation, Experiments, and In-
\nSitu Measurements<\/td>		Radio Science from Venus Probe\/Lander Mission<\/td>Robert Frampton<\/td>Boeing<\/td><\/td>\n<\/tr>\n
A8<\/td>II.1
\n<\/td>		Mars Exploration<\/td>Mars Exploration<\/td>InSight's Reconstructed Aerothermal Environments<\/td>Jarvis Songer<\/td> Lockheed Martin Space<\/td><\/td>\n<\/tr>\n
A9<\/td>II.2<\/td>Mars Exploration<\/td>Mars Exploration<\/td>Reconstruction of the Performance of Mars InSight Lander's Supersonic Parachute<\/td>Ian Clark<\/td>Jet Propulsion Laboratory, California Institute of Technology<\/td><\/td>\n<\/tr>\n
A10<\/td>II.3<\/td>Mars Exploration<\/td>Mars Exploration<\/td>Landing Radar Performance Reconstruction for Entry, Descent, and Landing of the
\nInSight Mars Lander<\/td>		Dave Eckart<\/td> Lockheed Martin Space<\/td><\/td>\n<\/tr>\n
A11<\/td>II.4<\/td>Mars Exploration<\/td>Mars Exploration<\/td>InSight Entry, Descent and Landing Operations Overview<\/td>Julie Wertz Chen<\/td> Jet Propulsion Laboratory, California Institute of Technology<\/td><\/td>\n<\/tr>\n
A12<\/td>II.5<\/td>Mars Exploration<\/td>Mars Exploration<\/td>InSight Entry, Descent, And Landing Post-Flight Simulation Assessment<\/td>Carlie Zumwalt<\/td>NASA Langley Research Center<\/td><\/td>\n<\/tr>\n
A13<\/td>II.6<\/td>Mars Exploration<\/td>Mars Exploration<\/td>InSight Landing Safety Assessment During Approach<\/td>Evgeniy Sklyanskiy<\/td> Jet Propulsion Laboratory, California Institute of Technology<\/td><\/td>\n<\/tr>\n
A14<\/td>II.7<\/td>Mars Exploration<\/td>Mars Exploration<\/td>Trajectory Analysis of the ExoMars Schiaparelli Descent Probe<\/td>Emma Johnstone<\/td>Fluid Gravity Engineering<\/td><\/td>\n<\/tr>\n
A15<\/td>II.8<\/td>Mars Exploration<\/td>Mars Exploration<\/td>Challenges For Mars 2020 EDL At The Jezero Crater Landing Site<\/td>Erisa Stilley<\/td> Jet Propulsion Laboratory, California Institute of Technology<\/td><\/td>\n<\/tr>\n
A16<\/td>II.9<\/td>Mars Exploration<\/td>Mars Exploration<\/td>AMELIA: The EDL Science Experiment For The Entry And Descent Module Of The
\nEXOMARS 2020 Mission<\/td>		Francesca Ferri<\/td>CISAS - Univ. Padova<\/td><\/td>\n<\/tr>\n
A17<\/td>II.10<\/td>Mars Exploration<\/td>Mars Exploration<\/td>Modelling Sensitivities and Knowledge Gaps Associated with Mars-atmosphere
\nDestructive Entry Applied to Planetary Protection<\/td>		James Merrifield<\/td>Fluid Gravity Engineering<\/td><\/td>\n<\/tr>\n
A18<\/td>II.11<\/td>Mars Exploration<\/td>Mars Exploration<\/td>Aerothermal Analysis and Thermal Protection System [TPS] Design of the Mars
\nSample Retrieval Lander [SRL] Concept<\/td>		Suman Muppidi<\/td> AMA Inc. at NASA Ames Research Center<\/td><\/td>\n<\/tr>\n
A19<\/td>II.12<\/td>Mars Exploration<\/td>Mars Exploration<\/td>ExoMars Rover and Surface Platform Mission: Technical Status<\/td>Andrew Ball<\/td>European Space Agency ESTEC<\/td><\/td>\n<\/tr>\n
A20<\/td>III.1<\/td>Sample Return to Earth<\/td>Sample Return to Earth<\/td>A Dynamic Topology Optimization Method for Sizing Internal Components of the Potential Mars Sample Return Earth Entry Vehicle<\/td>Cameron Grace<\/td>University at Buffalo<\/td>Student<\/td>\n<\/tr>\n
A21<\/td>III.2<\/td>Sample Return to Earth<\/td>Sample Return to Earth<\/td>Implementing CubeSat Avionics Components to Full-Scale Capsule Return Missions<\/td>Zachary Hughes<\/td>San Jose State University<\/td>Student<\/td>\n<\/tr>\n
A22<\/td>III.3<\/td><\/td><\/td><\/td><\/td><\/td><\/td>\n<\/tr>\n
A23<\/td>III.4<\/td>Sample Return to Earth<\/td>Sample Return to Earth<\/td>Structural Analysis of Impact-Tolerant Latched Containment Mechanisms for Mars Sample Return<\/td>Emma Shupper<\/td>Jet Propulsion Laboratory, California
\nInstitute of Technology<\/td>		<\/td>\n<\/tr>\n
A24<\/td>III.5<\/td>Sample Return to Earth<\/td>Sample Return to Earth<\/td>High Velocity Impact Performance of a Dual Layer Thermal Protection System for the Mars Sample Return Earth Entry Vehicle<\/td>Benjamin Libben<\/td>NASA Ames Research Center<\/td><\/td>\n<\/tr>\n
A25<\/td>IV.1<\/td>Innovative Concepts for Exploration<\/td>Innovative Concepts for Exploration<\/td>TOUTATIS-Ex: A CubeSat testbed for entry experiments on Mars<\/td>Chloe Gentgen<\/td>CentraleSup\u00e9lec<\/td>Student<\/td>\n<\/tr>\n
A26<\/td>IV.2<\/td>Innovative Concepts for Exploration<\/td>Innovative Concepts for Exploration<\/td>Lunar Gateway LASC Module for Innovative Concepts for Exploration: A Laserpowered Apparatus for Satellite Charging<\/td>Brandon Biggs<\/td>San Jose State University<\/td>Student<\/td>\n<\/tr>\n
A27<\/td>IV.3<\/td>Innovative Concepts for Exploration<\/td>Innovative Concepts for Exploration<\/td>Virtual Validation and Verification of the VaMEx Initative<\/td>Philipp Dittmann<\/td>University of Bremen<\/td>Student<\/td>\n<\/tr>\n
A28<\/td>IV.4<\/td>Innovative Concepts for Exploration<\/td>Modeling, Simulation, Testing, and Validation<\/td>Aerodynamic heating estimation of deployable inflatable aeroshell for Martian penetrator entry system<\/td>Tomoya Kazama<\/td>Tokyo University of Science<\/td>Student<\/td>\n<\/tr>\n
A29<\/td>IV.5<\/td>Innovative Concepts for Exploration<\/td>Modeling, Simulation, Testing, and Validation<\/td>Modal Analysis of the Orion Capsule Two Parachute System<\/td>Jing Pei<\/td>NASA Langley Research Center<\/td><\/td>\n<\/tr>\n
A30<\/td>IV.6<\/td>Innovative Concepts for Exploration<\/td>Modeling, Simulation, Testing, and Validation<\/td>Multi-Fidelity Modeling for Efficient Aerothermal Prediction of HIAD Configurations with Surface Scalloping<\/td>Mario Santos<\/td>Missouri University of Science and
\nTechnology<\/td>		Student<\/td>\n<\/tr>\n
A31<\/td>IV.7<\/td>Innovative Concepts for Exploration<\/td>Modeling, Simulation, Testing, and Validation<\/td>Deployable Mars Aero-Decelerators: Rib Deformation Modelling and Testing<\/td>Lisa Peacocke<\/td>Imperial College London \/ Airbus<\/td>Student<\/td>\n<\/tr>\n
A32<\/td>IV.8<\/td>Innovative Concepts for Exploration<\/td>Modeling, Simulation, Testing, and Validation<\/td>Modeling Thermal and Fluid Response of MMOD Impacted Thermal Protection Systems<\/td>Olivia Schroeder<\/td>University of Minnesota<\/td>Student<\/td>\n<\/tr>\n
A33<\/td>IV.9<\/td>Innovative Concepts for Exploration<\/td>Solar System Exploration II - Airless Planetary
\nSatellites, Asteroids, and Comets<\/td>		Enceladus Lander Mission Concept<\/td>Leora Peltz<\/td>Boeing<\/td><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n\n<\/div>\n","protected":false},"excerpt":{"rendered":"","protected":false},"author":2,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_monsterinsights_skip_tracking":false,"_monsterinsights_sitenote_active":false,"_monsterinsights_sitenote_note":"","_monsterinsights_sitenote_category":0,"footnotes":""},"class_list":["post-944","page","type-page","status-publish"],"_links":{"self":[{"href":"https:\/\/ippw2019.uk\/index.php\/wp-json\/wp\/v2\/pages\/944","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/ippw2019.uk\/index.php\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/ippw2019.uk\/index.php\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/ippw2019.uk\/index.php\/wp-json\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/ippw2019.uk\/index.php\/wp-json\/wp\/v2\/comments?post=944"}],"version-history":[{"count":4,"href":"https:\/\/ippw2019.uk\/index.php\/wp-json\/wp\/v2\/pages\/944\/revisions"}],"predecessor-version":[{"id":979,"href":"https:\/\/ippw2019.uk\/index.php\/wp-json\/wp\/v2\/pages\/944\/revisions\/979"}],"wp:attachment":[{"href":"https:\/\/ippw2019.uk\/index.php\/wp-json\/wp\/v2\/media?parent=944"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}