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  • IAC-25
  • B4
  • 5
  • session 5

    Title

    Access to Space for Small Satellite Missions

    type

    oral

    Description

    A key challenge facing the viability and growth of the small satellite community is affordable and reliable space access. Topics of interest for this session include the utilization of dedicated launches; development of ride-share systems, auxiliary payload systems, and separation and dispenser systems; and responsive integration approaches that will enable efficient small satellite access to space. Includes lessons learned from users on technical and programmatic approaches. For a dedicated discussion of small satellite propulsion systems, please refer to session B4.5A-C4.8. For a discussion of small launchers concepts and operations, please refer to session D2.7.

    Date

    2025-10-01

    Time

    15:00

    Room

    Room C3.2

    IPC members
    • Co-Chair: Mr. Yves Gerard, Airbus Defence & Space, France;

    • Co-Chair: Mr. Philip Davies, Surrey Satellite Technology Ltd (SSTL), United Kingdom;

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

    • Rapporteur: Mr. Carlos Niederstrasser, Northrop Grumman Corporation, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    Utilizing Small Satellite Launch Vehicle - A Cross-Border Collaboration for Space Mission Australia India Technology Research and Innovation (Space MAITRI) by Space Machines Company and New Space India Limited

    10

    Mr. Nhat Nguyen

    Space Machines Company

    Australia

    2

    15:10

    Enabling On-Demand Launches and Reentries

    10

    Mr. Zheng Tao

    United States

    3

    15:20

    Leveraging Innovative Launch Opportunities for Low-Cost Space Access

    10

    Dr. SANDhYA RAO

    India

    4

    15:30

    Very Low Earth Orbit Nanosatellite Platform with Innovative, Resource-Saving Orbit Keeping Strategy

    10

    Mr. Georg Langer

    Technische Universität Dresden (DTU)

    Germany

    5

    15:40

    Early Validation of a Small Satellite Design Guideline for Efficient Stacking in Heavy Launchers

    10

    Dr. Barnaby Osborne

    ESA

    United Kingdom

    6

    15:50

    Low cost cluster self reconfigurable modular spacecraft for multimodal space and ground observation missions

    10

    confirmed

    Mr. Tongshu Zhang

    Northwestern Polytechnical University;National Key Laboratory of Aerospace Flight Dynamics

    China

    7

    16:00

    Lesson Learned from Tracking & Identification for Rideshare LEOP Support

    10

    Mr. Robert Arthur

    NeuraSpace, SA

    United Kingdom

    8

    16:10

    Optimizing CubeSat Constellations for LEO Earth Observation: Maximizing Coverage and Revisit Capabilities

    10

    Ms. Tarifa AlKaabi

    Sharjah Academy for Astronomy, Space Sciences and Technology (SAASST)

    United Arab Emirates

    9

    16:20

    Constellation Reconfiguration and Task Scheduling Optimization for Emergency Earth Observation Response Using Low-Thrust

    10

    confirmed

    Mr. Zhengqing Fang

    Tsinghua University School of Aerospace

    China

    10

    16:30

    a fast-response launch planning method for small satellites

    10

    Ms. YAN LYU

    China Academy of Launch Vehicle Technology (CALT)

    China

    11

    16:40

    Ballistic coefficient characterization of the 3U CubeSat IGNIS mission

    10

    Mr. Corrado D'Urso

    University of Naples "Federico II"

    Italy

    12

    16:50

    In-space and Atmospheric Reentry Energy Generation with AMALTHEA – a CubeSat-Based Technology Demonstration

    10

    Ms. Maria Chytka

    University of Alabama in Huntsville

    United States

    13

    17:00

    Orbital Docking and Integration Nexus (ODIN): A Scalable and Sustainable in-orbit Platform for Space Research

    10

    Mr. Oliver Legon

    University of Nottingham

    United Kingdom

    *

    Aerodynamic Optimization and Hybrid Neuro-Fuzzy Logic Controller for Orbital Station-Keeping of CubeSats in VLEO

    10

    Mr. Vishwas Jajpura

    Indian Institute of Technology Kharagpur

    India

    *

    Opportunistic Space-Based Space Situation Awareness using Star Trackers

    10

    Ms. Hayley Richardson

    Inovor Technologies

    Australia