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  • 7
  • session 7

    Title

    Small Launchers: Concepts and Operations

    Description

    Discussion of existing, planned or future Small Launchers and On-orbit transfer systems for small payloads (from 500 kg to as low as 1 kg into Low Earth Orbit). Includes innovative solutions such as airborne systems, evolutions from sub-orbital concepts and flexible, highly reactive concepts. Includes piggy-back solutions based on larger launchers. Includes mission operations,associated operations and specific constraints. For a discussion of access to space for small satellite missions, please refer to session B4.5.

    Date

    2010-09-30

    Time

    15:15

    Room

    Chamber

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

    • Chairman: Mr. Shayne Swint, National Aeronautics and Space Administration (NASA), Marshall Space Flight Center, United States;

    • Rapporteur: Mr. Markus Jaeger, Airbus Defence & Space, Space Systems, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A Microsatellite Launch System using the XP Spaceplane as a Reusable First Stage for a New Generation Hybrid Rocket Upper Stage

    20

    confirmed

    Mr. Charles Lauer

    Rocketplane Global, Inc.

    United States

    2

    Japan pico nano advance launch system

    20

    confirmed

    Mr. Kazuhiro Yagi

    IHI Aerospace Co, Ltd.

    Japan

    3

    Light-gas gun launcher concept for high-g proof miniature suborbital payloads

    20

    confirmed

    Dr. Frank Schäfer

    Fraunhofer EMI

    Germany

    4

    Responsive, low-Cost Launch of Nanosatellites and Technology Demonstrations

    20

    confirmed

    Mr. Steve Cook

    Dynetics

    United States

    5

    Thrust Optimization and Operational Strategy for Low Earth Orbit Launch Vehicle

    20

    confirmed

    Mr. Jung-Woo Park

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    6

    Staging Mechanism Status of the Orbital Launcher NERVA

    20

    confirmed

    Prof. Radu Rugescu

    Politechnic University of Bucharest

    Romania

    7

    Robust Control for Air-Launched Systems

    20

    confirmed

    Mr. Luigi Ridolfi

    Scuola di Ingegneria Aerospaziale

    Italy

    8

    Modular Payload Deck Elements for Small Launch Vehicles

    20

    confirmed

    Mr. Abe Bonnema

    ISIS - Innovative Solutions In Space B.V.

    The Netherlands

    9

    Combustible Case, Mobile Engine and no Feed Device: the Concept of a Pico Launch Vehicle

    20

    Dr. Vitaly Yemets

    Dniepropetrovsk National University

    Ukraine

    10

    Dnepr program: reliability and innovations in service of small satellites

    20

    confirmed

    Mr. Alexander Serkin

    ISC Kosmotras

    Russian Federation