IAF Digital Library

10

session 10

Title: Propulsion Technology (3)
type: oral
Description: This session included all science and technologies supporting all aspects of space propulsion.
Date: 2017-09-29
Time: 11:00
Room: City Room 4

IPC members

Co-Chair: Mr. Norbert Puettmann, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;
Co-Chair: Prof. Riheng Zheng, Beihang University, China;
Rapporteur: Dr. Jerrol Littles, Aerojet Rocketdyne, United States;
Rapporteur: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Development of a Water Propulsion System for Small Satellites	15	confirmed	Mr. Nicholas Harmansa	IRS, University of Stuttgart	Germany
2		Analysis of the pressure surge during fast transient in evacuated spacecraft feedlines	15	confirmed	Mr. Cristiano Bombardieri	DLR (German Aerospace Center)	Germany
3		Numerical and Experiment Research of Nonsymmetric Cavitation Flow in Inducer During Head Drop	15	no-show	Mr. Longxian Li	Research & Development Center of China Academy of Launch Vehicle Technology	China
4		Influence of Coaxial Injector on High-frequency Combustion Instability for Staged Combustion LOX/kerosene Rocket Engine	15	withdrawn	Dr. Longfei Li	Northwestern Polytechnical University	China
5		The Experimental Investigation and On-orbit Flying Validation of an ADN-based Liquid Thruster	15	withdrawn	Dr. Zhaopu Yao	Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)	China
6		Catalyst Active Material Derivation for Ethanol-blended Hydrogen Peroxide Monopropellant Thruster	15	confirmed	Mr. Seungkwan Baek	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
7		Hypergolic Ionic Liquids as Green Propellants	15	confirmed	Ms. Anna Thomas	Stanford University	United States
8		NEA Scout Propulsion System Testing	15	withdrawn	Mr. Alber Douglawi	Purdue University	United States
9		Research on Thermal Decomposition of Hydrogen Peroxide For Low Thrust Propulsion System Application	15	confirmed	Dr. Lukasz Mezyk	Warsaw University of Technology (WUT)	Poland
10		Characterization of Selective Laser Melting Impinging Injectors	15'	confirmed	Mr. Deepak Atyam	Purdue University	United States
11		Advancement of Rocket Engine Performance through Novel Approaches for Thrust Chamber Design	15	confirmed	Mr. Markus Ortelt	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
12		Combustion dynamics in cryogenic rocket engines: research programme at DLR Lampoldshausen	15	confirmed	Dr. Justin Hardi	German Aerospace Center (DLR)	Germany
–		Characterization of Supercritical Properties in Atomization and Spray Characteristics of a Fuel Centred Pintle Injector in a 10kN Regenerative Cooled Pressure Fed Engine using Liquid Methane as Fuel	15'	withdrawn	Mr. Rohan M Ganapathy	Bellatrix Aerospace Private Limited	India