• Home
  • IAC Papers Archive
  • Public Website
  • Home
  • event
  • IAC-13
  • D2
  • 3
  • session 3

    Title

    Upper Stages, Space Transfer, Entry and Landing Systems

    Description

    Discussion of existing, planned or new advanced concepts for cargo and human orbital transfer. Includes current and near term transfer, entry and landing systems, sub-systems and technologies for accommodating crew and cargo transfer in space.

    Date

    2013-09-24

    Time

    14:45

    Room

    311B

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

    • Chairman: Dr. Oliver Kunz, RUAG Space, Switzerland;

    • Rapporteur: Dr. Gennaro Russo, Associazione Italiana di Aeronautica e Astronautica (AIDAA), Italy;

    papers

    Order

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    confirmed

    15'

    Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle

    Dr. Davide Cinquegrana

    CIRA Italian Aerospace Research Centre

    Italy

    2

    15'

    ATV Propulsion System - Welcome on board! How the ATV missions' feedback and real-time monitoring have been managed in a continuous improvement process

    Mr. Johann HENOCQUE

    Airbus DS GmbH

    Germany

    3

    withdrawn

    15'

    Mission Concept and Technical Subjects of HTV-R (HTV-Return)

    Mr. Yusuke Suzuki

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    confirmed

    15'

    CARAVAN Cargo Autonomous Rendezvous And Velocity Adjustment/Navigation

    Mr. Udrivolf Pica

    International Space University (ISU)

    Russian Federation

    5

    withdrawn

    15'

    A Study of Reentry Blackout Alleviation Using Electron Bunching in the Reentry Plasma Layer

    Mr. Siddharth Krishnamoorthy

    Student

    United States

    6

    confirmed

    15'

    Applied Magneto-aerodynamics for safer re-entry of space vehicle.

    Mr. Aakash Chhunchha

    SRM University, Chennai

    India

    7

    withdrawn

    15'

    Aerothermodynamics of an Optimal Design of Mars Re-Entry Vehicle from Hypersonic to Subsonic Flow Regime

    Mr. Balbir Singh

    Manipal Institute of Technology, Manipal University

    India

    8

    confirmed

    15'

    Modeling and Analyzing of the Soft-landing Phase of Parachute-Retrorocket System

    Mr. Huang Wei

    Beijing Institute of Mechanical & Electrical Engineering

    China

    9

    confirmed

    15'

    Scheme design of a parachute recovery system for UAV

    Dr. Jingqi Cai

    China Academy of Launch Vehicle Technology (CALT)

    China

    10

    15'

    Design philosophy for OTV operating on cryogenic propellant components

    Mr. Dmitry Loupiak

    Energia RSC

    Russian Federation

    11

    15'

    Space Launch System Evolvability Assessment: Upper Stage Definition

    Mr. Jon Holladay

    NASA

    United States