• Home
  • IAC Papers Archive
  • Public Website
  • My papers
  • 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

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

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

    15'

    confirmed

    Dr. Davide Cinquegrana

    CIRA Italian Aerospace Research Centre

    Italy

    2

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

    15'

    Mr. Johann HENOCQUE

    Airbus DS GmbH

    Germany

    3

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

    15'

    withdrawn

    Mr. Yusuke Suzuki

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    CARAVAN Cargo Autonomous Rendezvous And Velocity Adjustment/Navigation

    15'

    confirmed

    Mr. Udrivolf Pica

    International Space University (ISU)

    Russian Federation

    5

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

    15'

    withdrawn

    Mr. Siddharth Krishnamoorthy

    Student

    United States

    6

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

    15'

    confirmed

    Mr. Aakash Chhunchha

    SRM University, Chennai

    India

    7

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

    15'

    withdrawn

    Mr. Balbir Singh

    Manipal Institute of Technology, Manipal University

    India

    8

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

    15'

    confirmed

    Mr. Huang Wei

    Beijing Institute of Mechanical & Electrical Engineering

    China

    9

    Scheme design of a parachute recovery system for UAV

    15'

    confirmed

    Dr. Jingqi Cai

    China Academy of Launch Vehicle Technology (CALT)

    China

    10

    Design philosophy for OTV operating on cryogenic propellant components

    15'

    Mr. Dmitry Loupiak

    Energia RSC

    Russian Federation

    11

    Space Launch System Evolvability Assessment: Upper Stage Definition

    15'

    Mr. Jon Holladay

    NASA

    United States