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  • 5.-D2.7
  • session 5.-D2.7

    Title

    Joint Session: Small Spacecraft Launch, Injection, and Orbit Transfer Systems

    Description

    A key challenge facing the viability and growth of the small satellite community is affordable and reliable space access. This is achieved through small launchers, ride-shares, piggyback launches, and spacecraft propulsion technologies to reach final operational orbit. Topics of interest for this session include existing and conceptual launch platforms for small spacecraft; launcher and small spacecraft component and sub-system development that will enable efficient small spacecraft access to orbit and orbit change (e.g., propulsion systems, separation and dispenser systems, upper stages); and lessons learned from users on technical and programmatic approaches.

    Date

    2009-10-14

    Time

    15:00

    Room

    Technical Session #1

    IPC members
    • Chairman: Mr. Alex da Silva Curiel, Surrey Satellite Technology Ltd (SSTL), United Kingdom;

    • Rapporteur: Dr. Jeff Emdee, The Aerospace Corporation, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    2

    YUZHNOYE SDO-DEVELOPED SPACE ROCKET SYSTEMS INTENDED TO LAUNCH NANO AND MICRO SATELLITES

    15'

    Mr. Alexander Kushnarev

    Yuzhnoye State Design Office

    Ukraine

    3

    The Development of a Low Cost and Responsive Microsatellite Launch System using the XP Spaceplane as a Reusable First Stage

    15'

    Mr. Charles Lauer

    Rocketplane Global, Inc.

    United States

    4

    FlyMate: The Next Generation of Picosatellite Orbital Deployers

    15'

    Mr. Spas Balinov

    Novanano SAS

    France

    5

    Analysis of launch methods for small satellites

    15'

    Mr. Luca Mastrangelo

    University of Rome “La Sapienza”

    Italy

    6

    Results of the first stage development for the Romanian orbital launcher NERVA

    15'

    Prof. Radu Rugescu

    Politechnic University of Bucharest

    Romania

    7

    UKlaunch: Taking small satellites to orbit on the crest of the Space Tourism wave

    15'

    Dr. Adam Baker

    Rocket Engineering Ltd.

    United Kingdom

    9

    The major advantages, the preliminary system design and the LEO performance of a Small Launch Vehicle based on Hybrid Propulsion.

    15'

    Mr. Mauro Balduccini

    AVIO Propulsione Aerospaziale

    Italy

    10

    Development of the Propulsion Controller of the Hall Thruster for Science Technology Satellite-3 (STSAT-3)

    15'

    Mr. Sung-Ho Rhee

    Satellite Technology Research Center

    Korea, Republic of