session IP

Title: Interactive Presentations - IAF MATERIALS AND STRUCTURES SYMPOSIUM
type: interactive
Description: This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Materials and Structures addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific ten minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the C Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.
Date: 2022-09-21
Time: 13:30
Room: IP Area

IPC members

Co-Chair: Dr. Jochen Albus, ArianeGroup, Germany;
Co-Chair: Mr. Alwin Eisenmann, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;
Co-Chair: Ms. Coraline Dalibot, Rutherford Appleton Laboratory, United Kingdom;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
model based control of dexterous tensegrity robots	10	withdrawn	Mr. Nate Osikowicz	Pennsylvania State University	United States
Design for a Mars Rover with Enhanced Mobility to achieve Short-Term Flights: A Flying Rover	10	confirmed	Mr. Roshan Prince	ASTROPHYSICAST	India
Surviving the Lunar Night with Masten’s NITE™ System	10		Mr. Matthew Kuhns	Masten Space Systems	United States
Sharjah-Sat-1 Structural Design and Analysis	10	confirmed	Mrs. Maryam Alansaari	Sharjah Academy for Astronomy, Space Sciences and Technology (SAASST)	United Arab Emirates
Launch Environment Structural Survivability Verification for THEOS-2 SmallSat Structural Qualification Model (SQM) by Structural Dynamic Analysis and Vibration Testing.	10	confirmed	Mr. Panachai Santananukarn	Geo-Informatics and Space Technology Development Agency (GISTDA)	Thailand
High-Performance polyimide membranes for use in solar sail propulsion	10	confirmed	Dr. Elisa Toto	Sapienza University of Rome	Italy
Finite time fault-tolerant control and multiple vibration suppression of space robot with elastic base, elastic joints and flexible links	10	confirmed	Dr. Haiping Ai	Fuzhou University	China
Research on the heating effects of the main engine jet of the suborbital vehicle	10	confirmed	Dr. Xiaoyan Li	CASC	China
Design of interstage structures transferring thrust from booster to core stage of ISRO missions - a paradigm shift	10	confirmed	Mr. Sirajudeen Ahamed S	Indian Space Research Organization (ISRO)	India
Chassis Optimization of a 1U Cubesat made in a developing country	10	confirmed	Mr. Wenceslao Bejarano	National Autonomous University of Honduras (UNAH)	Honduras
Design process and new materials in small satellite structures	10	confirmed	Mr. Edwin Cruz Martínez		Mexico
Research on the analysis of drilling behavior to minimize delamination in carbon fiber reinforced plastics	10	confirmed	Mr. Sirapop Mongkolves	National Astronomical Research Institute of Thailand (NARIT)	Thailand
Compilation method of equal damage accelerated fatigue load spectrum for reusable launch vehicle	10	confirmed	Dr. Sichao Deng	China Academy of Launch Vehicle Technology (CALT)	China
Optimal sensor placement of rotor-bearing system based on fault diagnosability	10	confirmed	Mr. liu yuwei	National University of Defense Technology	China
Determination of Thruster Configuration and Experimental Verification for Buoyant Rover Concept	10	confirmed	Mr. Roy Ramirez		Costa Rica
Origami-inspired deployable solar reflectors for mission lifetime extension of robotic vehicles for lunar exploration	10	confirmed	Mr. Vipul Mani	TU Berlin	Germany
On the vibration testing of space structures	10	confirmed	Dr. Nikolay Asmolovskiy	Space Structures GmbH	Germany
Methods of increasing the efficiency of a detonation jet engine running on environmentally friendly fuel.	10		Mr. Vitalii Stoliarchuk	State Enterprise M.K. Yangel “Yuzhnoye” Design Office	Ukraine
Viability and Advantages of Graphene Production in Deep Space Environment	10	withdrawn	Mr. Paul Kiesling	BLUECUBE Aerospace	United States
Mechanical Analysis of a Novel Cylindrical Langmuir Probe Module of CubeSat under Launch Vibration Environment	10	confirmed	Dr. Shankar Bhattarai	Korea Astronomy and Space Science Institute	Korea, Republic of
CFD Analysis and Experimental Verification of Kraft Paper body tube for Sounding Rockets	10	confirmed	Mr. Advaith P Shetty	R V College of Engineering, Bengaluru	India
Design assessment of gimbal bellows used in a cryogenic rocket stage using experiments and numerical methods	10	confirmed	Mr. Unnikrishnan K R	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
Testing and Manufacturing of a Hypersonic Rocket Fins	10	confirmed	Mr. Mohammed Omar Nawaz	Concordia University	Canada
Design & Experimental Demonstration of a Rigid Suspension System for Lunar Micro-roving	10	confirmed	Ms. Lydia Schweitzer	Carnegie Mellon University	United States
Computer aid simulation to obtain internal stress from static and random vibration analysis of the 1U k'oto nano satellite.	10	confirmed	Mr. Sergio Rios Rabadan	High Technology Unit (UAT) Faculty of Engineering - UNAM	Mexico
Structure redesign for the nanosatellite K’oto	10	confirmed	Ms. María Guadalupe Ortega Ontiveros	Facultad de Ingeniería-UNAM	Mexico
Innovation in water rockets development based on biomimicry design tools in collaboration with the Aerospace Engineering Group of Universidad de Costa Rica (UCR)	10	confirmed	Ms. Angely Dittel	Universidad de Costa Rica	Costa Rica
Design of a device to slow the motion and vertical descent of a water rocket inspired by tropical seeds from Costa Rica	10	confirmed	Mr. Francisco Eduardo Salazar Lopez	University of Costa Rica	Costa Rica
VI-STAR: Variable Insulation System for Thermal Active Regulation	10	confirmed	Ms. Apoorva Joshi		India
Thermal Control Design of Cabin Type for Star Sensor on GEO Satellite	10	confirmed	Mr. Han Chongwei	China Academy of Space Technology (CAST)	China
Layout candidate schemes for small Satellite based on multi-objective optimization algorithm	10	confirmed	Mr. Anuphong Sangthon	National Astronomical Research Institute of Thailand (NARIT)	Thailand
Structural assessment of Solid Rocket Motor hardware from the measured residual strain and 3-D profile in the long seam weld location	10	confirmed	Mr. Paul Murugan J	Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram	India
Development of a novel biodesign approach in the construction of habitats both here on Earth and on other celestial bodies, based upon the core principles of functionality and environmental sustainability.	10	withdrawn	Dr. Amy Holt	International Space University (ISU)	United Kingdom
Small rockets design using Additive Manufacturing: An Educational Approach.	10	confirmed	Mr. Irving Enrique Gomez Fernandez		Mexico
High-performance thermoplastic composite structure for suborbital vehicles	10	confirmed	Mr. Daniele Tortorici	Sapienza University of Rome	Italy
Experimental and Numerical Investigation of Spread Tow Fabric Composites for Boom Application	10	confirmed	Ms. Flavia Palmeri	Sapienza University of Rome	Italy
A simplified thermal analysis for Thai Space Consortium-1 satellite (TSC-1)	10	confirmed	Mr. Chinathip Narongphun	National Astronomical Research Institute of Thailand (NARIT)	Thailand
Preliminary Study of an Origami-inspired Deployable Structure for a Small-scale Demonstrator	10	confirmed	Ms. Ines Uriol Balbin	Delft University of Technology (TU Delft)	The Netherlands
Cryogenic behaviour of Airware 2050 Aluminium alloy: application for space products down to LH2 environment	10	confirmed	Dr. David Cardinaux	Aubert & Duval	France
Prediction of braze joint strength of dissimilar materials by numerical and experimental methods.	10	confirmed	Mr. Anoop Kumar A	Indian Space Research Organization (ISRO)	India
Development and vibration analysis of an on-orbit 3D printer	10		Mr. Amin Motahari	Carleton Univeristy	Canada

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