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  • 7
  • session 7

    Title

    Suborbital Rockets and Small Launchers: Concepts and Operations including Student Rocketry

    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 considering also student rocketry technical achievements for the development of their sounding rockets: development of subsystems, safety issue, uses of novel technologies

    Date

    2025-10-02

    Time

    15:00

    Room

    Room C4.1

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

    • Co-Chair: Mr. Christian Corba, EUMETSAT, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    Smallsats by the Numbers 2024: Growing Smallsat Activity and its Implications for the Small Launch

    15

    Mr. Nickolas Boensch

    Bryce Space and Technology

    United States

    2

    15:15

    design of a supersonic sounding rocket to the stratosphere

    15

    Mr. Patrick Underwood

    RMIT University

    Australia

    3

    15:30

    harnessing suborbital capabilities: key takeaways from the ilr-33 amber 2k test flight

    15

    Mr. Michal Pakosz

    Łukasiewicz Research Network – Institute of Aviation (ILOT)

    Poland

    4

    15:45

    Multistage rocket: technological validation for space access in Mexico

    15

    Mr. Julio Alberto Cardenas Hernandez

    Universidad Nacional Autónoma de México (UNAM)

    Mexico

    5

    16:00

    predicting the flight paths and apogee of a sounding rocket

    15

    Ms. Tamzin Magyar

    RMIT University (Royal Melbourne Institute of Technology)

    Australia

    6

    16:15

    System-Level Optimization and Validation of a Small Suborbital Launch Vehicle with Rocket and Jet Propulsion

    15

    confirmed

    Mr. Shinhyung Kim

    Chosun University

    Korea, Republic of

    7

    16:30

    The ALDUINA Hybrid Upper Stage: Propulsion System Design and Support Infrastructure

    15

    Mr. Andrija Dabanovic

    German Aerospace Center (DLR)

    Germany

    8

    16:45

    Pioneering the Skies: The Future of Suborbital Rockets and Small Launchers

    15

    confirmed

    Ms. Raneem Alazzam

    Jordan University of Science & Technology

    Jordan

    9

    17:00

    FLEXIABLE NANO LAUNCH VEHICLE SYSTEM

    15

    Mr. Mehmet Fatih Engin

    University of Turkish Aeronautical Association

    Türkiye

    10

    17:15

    Advancing Suborbital Rockets and Small Launchers: Concepts, Operations, and Student Rocketry

    15

    Mr. Dheerajprabhu S

    India

    11*

    17:30

    design and optimization of propeller-based thrust vector control mechanism using pid and sensor fusion techniques

    15

    Mr. Abdulla Hil Kafi

    Kyushu Institue of Technology

    Japan

    12*

    17:30

    Development and Testing of Low-Cost Ablative Composites for Student-Built Liquid Rocket Engines

    15

    Mr. Dheerajprabhu S

    India