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  • session 6

    Title

    Space Environmental Effects and Spacecraft Protection

    type

    oral

    Description

    The focus of the session will be on space environmental effects and spacecraft protection. The effects of vacuum, radiation, atomic oxygen, spacecraft charging, thermal cycling, dissociation, meteoroids and space debris impact on space systems, materials and structures, and microelectronics will be addressed. Protective and shielding technologies, including analysis simulation and testing of debris impact, and susceptibility of Commercial-Off-The-Shelf (COTS) micro-electronics to space radiation will be covered.

    Date

    2015-10-15

    Time

    09:45

    Room

    Oranim 1 (ICC, lower level)

    IPC members
    • Co-Chair: Dr. Giuliano Marino, CIRA Italian Aerospace Research Centre, Italy;

    • Rapporteur: Mr. Anatolii Lohvynenko, Yuzhnoye State Design Office, Ukraine;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    SPACE RADIATION HARDNESS ASSURANCE OF A SATELLITE WITH THE USE OF PROTECTIVE MATERIALS SPACE RADIATION HARDNESS ASSURANCE OF A SATELLITE WITH THE USE OF PROTECTIVE MATERIALS

    12'

    confirmed

    Mr. Oleg Dotsenko

    Yuzhnoye State Design Office

    Ukraine

    2

    Heat flux sensor for spacecraft charging thermal protection

    12'

    confirmed

    Prof. Aleksey V. Nenarokomov

    Moscow Aviation Institute

    Russian Federation

    3

    Atomic Oxygen Exposure Testing of Novel Layered POSS Thermoset Nanocomposites

    12'

    confirmed

    Ms. Jessica Piness

    University of Southern Mississippi

    United States

    4

    RoBiSat Mission: Double Unit CubeSat Thermal analysis in context of QB50 mission

    12'

    confirmed

    Mr. Mugurel Balan

    Institute of Space Science

    Romania

    5

    Temperature monitoring of thermal-vacuum tests with optical fiber sensors.

    12'

    confirmed

    Mr. Claudio Paris

    Sapienza University of Rome

    Italy

    6

    CMOS SENSOR AS IONIZING RADIATION DETECTOR AND THERMOLUMINESCENCE RESPONSE

    12'

    confirmed

    Mr. Yair Israel Piña López

    Universidad Nacional Autónoma de México

    Mexico

    7

    A cost effective approach for qualifying commercial hardware for low-earth-orbit applications

    12'

    withdrawn

    Mr. Torsten Koehne

    OHB System AG-Bremen

    Germany

    8

    The effects of space environment on thermo-optical degradation of solar sail material

    12'

    confirmed

    Prof. Roman Ya. Kezerashvili

    New York City College of Technology, The City University of New York

    United States

    9

    Active and passive protection of Low Earth Orbit satellites from space environmental effects

    12'

    confirmed

    Mr. Akash Paliya

    Manipal Institute of Technology, Manipal University

    India

    10

    Mission Optimization of High-Speed Entry Flight Test for Deep Space Exploration Vehicles

    12'

    no-show

    Dr. Wenrui Wu

    Institute of Manned Space System Engineering,China Academy of Space Technology (CAST)

    China

    11

    thermal expansion properties of carbon fiber reinforced PEEK unidirectional prepreg

    12'

    confirmed

    Mr. jianping han

    Xi'an Aerospace Composites Materials Institute

    China

    12

    GC-MS and IR spectrometry analyses for component identification of materials outgassing contamination of spacecraft

    12'

    no-show

    Dr. Zi-long Jiao

    Beijing Institute of Spacecraft Environment Engineering

    China