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  • session 4

    Title

    Solid and Hybrid Propulsion (2)

    Description

    This session includes all science and technologies supporting all aspects of solid and hybrid propulsion.

    IPC members
    • Co-Chair: Mr. Jerome Breteau, European Space Agency (ESA), France;

    • Co-Chair: Mr. Jean-Claude Traineau, Office National d’Etudes et de Recherches Aérospatiales (ONERA), France;

    • Rapporteur: Dr. Arif Karabeyoglu, Koc University, Turkey;

    • Rapporteur: Mr. Ozan Kara, Space Generation Advisory Council (SGAC), Turkey;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A Novel Coordinated Energetic Compound Leading a Promising Concept of Propellant Formula Designing

    15

    confirmed

    Mr. Zhenhao Mi

    The 41st Institute of the Fourth Academy, China Aerospace Science and Technology Corporation (CASC)

    China

    2

    Energetic hybrid rocket propellants for upper stage propulsion

    15

    confirmed

    Mr. Vinayak Malhotra

    SRM University Chennai

    India

    3

    Performance evaluation of modified loose flap venting scheme introduced for the propellant processing of upper stage SRM through hot test

    15'

    confirmed

    Mr. Shubham Maurya

    Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram

    India

    4

    Experimental Parametric Study of Rocket Grain Configuration on Potassium Nitrate Propellant with Additives employing Rocket Motor Design Computational Fluid Dynamics

    15

    Ms. Kirti Vishwakarma

    University of Petroleum and Energy Studies

    India

    5

    Development of a Thrust Control System for Rocket Engines

    15

    confirmed

    Mr. Maurício Gontijo

    University of Brasilia

    Brazil

    6

    Experimental and Numerical Study on Feasibility of 5kN Thrust Level Hybrid Rocket Motor using the Low-Melting-Point Thermoplastic Fuel

    15

    confirmed

    Dr. Yo Kawabata

    Japan

    7

    numerical and experimental research on ablation performance of a carbon/carbon composties solid rocket motor nozzle insert

    15

    confirmed

    Dr. Lin Sun

    Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University

    China

    8

    Experimental investigation on the anti-ablation properties of multi-material interface nozzle insert in hybrid rocket motors

    15

    Mr. Ruipeng Yu

    Beihang University

    China

    9

    Design and Optimization of a Scalable Hybrid Rocket Motor

    15

    confirmed

    Mr. Diego Talavera

    Luleå University of Technology

    Sweden

    10

    Hybrid Propulsion Motor Optimization for Application as Small Launcher Upper Stage to Support LEO Missions.

    15

    confirmed

    Mr. Anand Kumar Singh

    Department of Space Engineering, Lulea University of Technology

    Sweden

    11

    Study on thermoacoustic oscillation characteristics of carbon nanotubes

    15

    confirmed

    Mr. Yu Liao

    Northwestern Polytechnical University

    China

    12

    Performance of a solid propellant trans-media ramjet: a theoretical analysis

    15

    withdrawn

    Dr. Liya Huang

    National University of Defense Technology

    China

    13

    Experimental investigation of a flow-oriented throttleable injector designed for throttleable hybrid rocket motor

    confirmed

    Mr. Zeng Zhao

    School of Astronautics, Beihang University

    China

    14

    modeling and numerical simulation of thermal erosion in a toroidal aerospike nozzle

    confirmed

    Mr. Renan Almeida

    Universidade de Brasília

    Brazil

    15

    Using Lagrangian Coherent Structures to investigate flow field of the hot stage separation of a multistage rocket

    Dr. Jiahui Chen

    Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University

    China