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  • session 7

    Title

    Small Launchers: Concepts and Operations

    type

    oral

    Description

    Discussion of existing, planned and future Launchers for small payloads ranging from 1500 kg to as low as 1 kg into Low Earth Orbit. Includes innovative solutions such as airborne systems, evolutions from sub-orbital concepts, combinations of existing / emerging elements and new elements, reusable, partially reusable and expendable concepts, and flexible, highly responsive concepts. Includes mission operations, design, development, and specific constraints. For discussion on small satellite missions not focused on launchers and their operations, please refer to session B4.5.

    Date

    2017-09-26

    Time

    14:45

    Room

    Hall O

    IPC members
    • Co-Chair: Mr. Nicolas Bérend, ONERA - The French Aerospace Lab, France;

    • Co-Chair: Mr. Harry A. Cikanek, National Oceanic and Atmospheric Administration (NOAA), United States;

    • Rapporteur: Mr. Julio Aprea, European Space Agency (ESA), France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    LauncherOne: Responsive Launch for Small Satellites

    15

    confirmed

    Ms. Sirisha Bandla

    Virgin Galactic L.L.C

    United States

    3

    First results of the H2020 ALTAIR project – Towards an innovative cost-effective air launch system for small satellites

    15

    confirmed

    Mr. Nicolas Bérend

    ONERA - The French Aerospace Lab

    France

    4

    Fly Back Booster Design for Mach 5 Scramjet Launch

    15

    confirmed

    Mr. Joseph Chai

    University of Queensland

    Australia

    5

    Small Innovative Launcher for Europe: Achievement of the H2020 project SMILE

    15

    confirmed

    Mr. Bertil Oving

    Netherlands Aerospace Centre (NLR)

    The Netherlands

    6

    Trajectory design of sounding rocket based Nano launcher

    15

    confirmed

    Dr. Takayuki Yamamoto

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    10

    Development and Operation of a Hydrocarbon Liquid Propellant Orbital/Sub-Orbital Launcher

    15

    confirmed

    Mr. Ryuichiro KANAI

    Interstellar Technologies Inc.

    Japan

    12

    Conceptual Design Analysis for a Two-Stage-to-Orbit Semi-Reusable Launch System for Small Satellites

    15

    confirmed

    Dr. Christie Maddock

    University of Strathclyde

    United Kingdom