session 7

Title

Space Vehicles – Mechanical/Thermal/Fluidic Systems

Description

The topics to be addressed include novel technical concepts for mechanical/thermal/fluidic systems and subsystems of launchers, manned and unmanned spacecraft, re-entry vehicles and small satellites. Advanced subsystems and design of future exploration missions will be covered, considering issues arising from material selection, cost efficiency and reliability, and advancements in space vehicle development with respect to engineering analysis, manufacturing, and test verification.

Date

2013-09-26

Time

14:45

Room

306B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Parametric Shape Optimization of Reentry Module for Space Missions

accepted

15'

Dr. Ugur Guven

United States

2

Thermal modeling of the adaptive thermal control microsystem of the spacecraft

accepted

15'

confirmed

Mr. Anatoliy Patsievskiy

S.P. Korolev Rocket and Space Corporation Energia

Russian Federation

3

Global error estimation in CFD mesh coarsening process for uncertainty quantification methods

accepted

15'

confirmed

Mr. Martin Kubicek

University of Strathclyde

United Kingdom

4

Cooling system for high energy potential space vehicle

accepted

15'

confirmed

Mr. Anton Burdanov

Central Research Institute for Machine Building (JSC TSNIIMASH)

Russian Federation

5

Heat Transfer Management by Aerospikes for a Hypothesized Lifting Body in Hypersonic Flow

accepted

15'

withdrawn

Dr. Shashank Khurana

The University of TOKYO, Graduate school

China

6

aerodynamic improvement of the brazilian satellite launch vehicle

accepted

10'

confirmed

Mr. Col. Jose Duarte

Instituto de Aeronáutica e Espaço (IAE)

Brazil

7

Numerical study of active cooling techniques of a nano satellite using CFD for performance enhancement

accepted

10'

confirmed

Mr. Mollik Nayyar

Manipal Institute of Technology, Manipal University

India

8

Aerodynamic Design of a Capsule Configuration for High-speed Manned Re-entry

accepted

10'

confirmed

Mr. Bingyan Chen

China Academy of Aerospace Aerodynamics (CAAA)

China

9

variable inertia fluidic ring actuator on attitude control and residual fuel management systems

accepted

10'

confirmed

Ms. Hong Guan

Beihang University

China

10

the study on iot based manufacturing system for astronautical products

accepted

10'

confirmed

Mr. Xie Xinping

Nanjing University of Aeronautics and Astronautics

China

11

Thermal Mapping and Trends of Mars Analog Materials in Sample Acquisition Operations Using Experimentation and Models

accepted

10'

confirmed

Mr. Timothy Szwarc

Stanford University

United States

12

Transient study about the heat transfer of sublimator combined with fluid loop

accepted

10'

confirmed

Dr. Yuying WANG

Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology

China

13

Materials surface emissivity analyses performed by the combined use of dual and single color optical pyrometers

accepted

10'

confirmed

Dr. Carlo Purpura

CIRA Italian Aerospace Research Centre

Italy