session 8

Title: Advanced and Combined Propulsion Systems
type: oral
Description: The session is for the presentation of advanced propulsion concepts being studied or considered. The advanced concepts should seek to deliver breakthroughs in overcoming the limitations of propulsion systems in current use or development. For advanced concepts technologies should normally be in the range TRL 0 to TRL 2. Advanced concepts with higher TRL technologies may also be presented where a combination of propulsion technologies can lead to performance breakthroughs which can not be achieved with a single technology. A combination can include for example both chemical and electric or solid and liquid chemical.
Date: 2013-09-27
Time: 13:30
Room: 208A

IPC members

Chairman: Mr. Jacques Gigou, European Space Agency (ESA), France;
Chairman: Mr. Richard Blott, British Interplanetary Society, United Kingdom;
Rapporteur: Mr. William W. Smith, Aerojet Rocketdyne, United States;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	radio wave and ion cyclotron thruster	15'	confirmed	Mr. Harshit Bisen	SRM University Chennai	India
2	A NOVEL COMBINED PROPULSION CONCEPT FOR DEEP SPACE MISSIONS	15'	confirmed	Ms. Ragini Ramachandran	Embry-Riddle Aeronautical University	United States
3	FAST Z-PINCH THRUSTER FOR SPACE TUGS	15'	confirmed	Mr. Patrick Giddens	UAHuntsville	United States
4	Experimental tests of the Mach Effect Thruster.	15'	confirmed	Prof. Heidi Fearn	California State University	United States
5	ADVANCED SOLAR THERMAL PROPULSION WITH SPECTRAL-SELECTIVE MULTI-STAGED CONCENTRATOR-ABSORBER SYSTEM	15'		Prof. Oleg Kudrin	Moscow Aviation Institute	Russian Federation
5	ADVANCED SOLAR THERMAL PROPULSION WITH SPECTRAL-SELECTIVE MULTI-STAGED CONCENTRATOR-ABSORBER SYSTEM	15'		Prof. Sergey Finogenov	Moscow Aviation Institute	Russian Federation
6	Investigation on Status and Prospective Application of Gelled Propellants	15'	confirmed	Dr. Shuang Liu	The 41st Institute of the Sixth Academy of Aerospace Science & Industry Corp	China
7	A Study of Laser propulsion: An Overdriven detonation mode for a laser-absorption wave	15'	withdrawn	Mr. Joseph Ofosu	University of Tokyo	Japan
8	Numerical study on working processes of a novel laser ablation thruster with electromagnetic acceleration	15'		Mr. Daixian Zhang	College of Aerospace Science and Engineering, National University of Defense Technology	China
9	LightForce: Refined Laser Propulsion Force Model	15'	withdrawn	Mr. Fan Yang Yang	National Aeronautics and Space Administration (NASA), Ames Research Center / USRA	United States
10	Experimental Research on Continuous Detonation Engine	15'		Mr. Tianyi Shi	Peking University Health Science Center	China
11	Effects of Different Types of Diverging Nozzle on Propulsion Performance of Continuous Detonation Engine (CDE)	15'		Dr. Ugur Guven		United States
12	optimum control of ramjets at high flight Mach number and wide-range working conditions	15'	confirmed	Ms. Baoe Yang	Xi'an Aerospace Propulsion Institute	China

session 8

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