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  • session 3

    Title

    Upper Stages, Space Transfer, Entry and Landing Systems

    Description

    Discussion of existing, planned or new advanced concepts for cargo and human orbital transfer. Includes current and near term transfer, entry and landing systems, sub-systems and technologies for accommodating crew and cargo transfer in space.

    Date

    2009-10-13

    Time

    15:00

    Room

    Technical Session #2

    IPC members
    • Chairman: Dr. Luigi Bussolino, Bussolino and Associates, Italy;

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

    • Rapporteur: Mr. Ivan Bekey, Bekey Designs, Inc., United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Origin and Evolution of Orion Service Module Propulsion from ESAS to Initiation of Preliminary Design

    15'

    Mr. Harry A. Cikanek

    National Oceanic and Atmospheric Administration (NOAA)

    United States

    2

    Altair Lunar Lander Development Status: Enabling Human Lunar Exploration

    15'

    Mrs. Kathy Laurini

    National Aeronautics and Space Administration (NASA)

    United States

    3

    LANDING WITH SOLID PROPELLANT RETRO ROCKETS

    15'

    Mr. Philippe Augros

    EADS Space

    France

    5

    Reentry and Landing Guidance for Reusable Sounding Rocket

    15'

    Dr. Takayuki Yamamoto

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    6

    Thermal Protection System for long-term in-orbit cryogenic propellant storage

    15'

    Mr. Piotr Perczynski

    MT Aerospace AG

    Germany

    7

    Stepped development approach to HTV evolved spaceship

    15'

    Dr. Ko Ogasawara

    Mitsubishi Heavy Industries, Ltd.

    Japan

    8

    The Interaction Between Skylon and the International Space Station

    15'

    Mr. Mark Hempsell

    Reaction Engines Ltd.

    United Kingdom

    9

    Systematic Assessment of Advanced “Sharp-Edged” Lifting Body Re-entry Configurations

    15'

    Dr. Martin Sippel

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    10

    trajectory design for earth-moon orbital transfer using multiobjective genetic algorithm

    15'

    Mr. Mohammad Reza Farmani

    K. N. Toosi University of Technology

    Iran

    11

    Spacecraft Insertion into Earth-Moon L1 and Lunar Orbit

    15'

    Prof. Mikhail S. Konstantinov

    Moscow Aviation Institute

    Russian Federation

    12

    Trajectory Planning and Monte Carlo Simulation of Re-entry Vehicle during A/L Phase

    15'

    Mr. CHANOH MIN

    Pusan National University

    Korea, Republic of

    13

    The research of multi-satellite deploying method for upper stage

    15'

    Mr. junfeng wang

    China Academy of Launch Vehicle Technology (CALT)

    China