scholarly journals Test Facilities in Support of High Power Electric Propulsion Systems

2003 ◽  
Author(s):  
Melissa Van Dyke
Keyword(s):  
High Power ◽  
Electric Propulsion ◽  
Propulsion Systems

scholarly journals Structures of high-power electric propulsion systems

2021 ◽  
Vol 1 (395) ◽  
pp. 119-131
Author(s):  
I. Gagarinov ◽  
Keyword(s):  
Comparative Analysis ◽  
High Power ◽  
Electric Propulsion ◽  
Propulsion Systems ◽  
Technical Data ◽  
Electric Propulsion System ◽  
Design Solutions ◽  
Oil Tankers ◽  
Made In

Object and purpose of research. This paper discusses structures of high-power electric propulsion systems for ships. The purpose was to give a summary of design solutions made in development of these systems. Materials and methods. This paper relies on academic and technical data, as well on the long-term author’s experience in marine electric propulsion R&Ds. The solution suggested by the author is based on the comparative analysis of design solutions adopted in the development of structures for high-power marine electric power and propulsion systems. Main results. Summary on design solutions for high-power electric propulsion systems of such ships as icebreakers, oil tankers, LNGCs and cruise liners. Conclusion. Results obtained by author were used in the design of the electric propulsion system of the «Lider» nuclear icebreaker and further could be used in design of Arctic vessels.

scholarly journals Overview of Propulsion Systems for Unmanned Aerial Vehicles

Energies ◽  
2022 ◽  
Vol 15 (2) ◽  
pp. 455
Author(s):  
Bowen Zhang ◽  
Zaixin Song ◽  
Fei Zhao ◽  
Chunhua Liu
Keyword(s):  
Power Density ◽  
High Power ◽  
Electric Propulsion ◽  
Development Trend ◽  
Propulsion System ◽  
High Power Density ◽  
Propulsion Systems ◽  
Essential Information ◽  
Development Framework ◽  
Future Technologies

Unmanned Aerial Vehicle (UAV) propulsion technology is significantly related to the flight performance of UAVs, which has become one of the most important development directions of aviation. It should be noted that UAVs have three types of propulsion systems, namely the fuel, hybrid fuel-electric, and pure electric, respectively. This paper presents and discusses the classification, working principles, characteristics, and critical technologies of these three types of propulsion systems. It is helpful to establish the development framework of the UAV propulsion system and provide the essential information on electric propulsion UAVs. Additionally, future technologies and development, including the high-power density motors, converters, power supplies, are discussed for the electric propulsion UAVs. In the near future, the electric propulsion system would be widely used in UAVs. The high-power density system would become the development trend of electric UAVs. Thus, this review article provides comprehensive views and multiple comparisons of propulsion systems for UAVs.

scholarly journals A Facility for Testing High-Power Electric Propulsion Systems in Space - A Design Study

2005 ◽  
Author(s):  
Andrew Petro ◽  
Franklin Chang-Diaz ◽  
Charles Sarmiento ◽  
Greg Chavers ◽  
Neil Lemmons ◽  
...  
Keyword(s):  
High Power ◽  
Electric Propulsion ◽  
Design Study ◽  
Propulsion Systems

Evaluation of TAL technology applicability to high power (10 kW and above) electric propulsion systems

2001 ◽  
Author(s):  
Sergey Tverdokhlebov ◽  
Alexander Semenkin ◽  
Boris Shoumkin ◽  
Anatolii Kochergin ◽  
Bill Butler ◽  
...  
Keyword(s):  
High Power ◽  
Electric Propulsion ◽  
Propulsion Systems

scholarly journals High-power inductive electric propulsion operation with alternative propellants

2019 ◽  
Vol 124 (1272) ◽  
pp. 151-169 ◽  
Author(s):  
A. R. Chadwick ◽  
B. Dally ◽  
G. Herdrich ◽  
M. Kim
Keyword(s):  
Experimental Data ◽  
High Power ◽  
Electric Propulsion ◽  
Specific Impulse ◽  
Chemical Properties ◽  
Propulsion Systems ◽  
Experimental Campaign ◽  
Discharge Volume ◽  
Near Future ◽  
Maximum Thrust

ABSTRACTThis paper presents the results of an experimental campaign to measure thruster-relevant parameters for a high-power (180kW) inductive propulsion system utilising Ar, $ {\textrm{O}}_{2}$ , $ \textrm{N}_{2}$ , and $ \textrm{CO}_{2}$ as propellants. Results from the investigation show that inductive thrusters can make use of these propellants without the severe degradation seen in other electric propulsion systems. Furthermore, the collection of experimental data at powers greater than 100kW provides a reference of performance for the high-power electric propulsion devices intended for missions in the near future. Thrust and specific impulse in inductive systems can be improved by preferentially combining the chemical properties of atomic and molecular propellants. The maximum thrust recorded during these experiments was 7.9N, obtained using a combination of argon and oxygen (0.68 Ar + 0.32 $\textrm{O}_{2}$ ). The combination of argon and molecular propellants also decreased thermal losses within the discharge volume. Specific impulse can be doubled for the same input electric power by combining propellants, and future modifications to the thruster geometry and acceleration mechanism can be used to further improve the performance of such systems.

TRADEOFF ANALYSIS OF HIGH-POWER ELECTRIC PROPULSION SYSTEMS BASED ON DOMESTIC ELECTRIC PROPULSION ENGINES AND POTENTIAL FOR THEIR USE IN ORBIT-TO-ORBIT TRANSFER SYSTEMS AND DEEP SPACE EXPLORATION

2019 ◽  
pp. 45-55
Author(s):  
Yu.G. GUSEV ◽  
A.V. PILNIKOV ◽  
S.E. SUVOROV
Keyword(s):  
High Power ◽  
Electric Propulsion ◽  
Storage System ◽  
Current Status ◽  
Vacuum System ◽  
Deep Space ◽  
Propulsion Systems ◽  
Orbit Transfer ◽  
Rocket Propulsion ◽  
Component Development

The paper discusses design solutions for increased-power and high-power electric rocket propulsion systems to be used in orbit-to-orbit transfer vehicles and advanced spacecraft. It reviews characteristics of their components from the standpoint of the mission to reboost the spacecraft to their target orbits, to perform the operations of transportation to the lunar orbit and to explore deep space. It discusses key criteria and procedures for selection of components, as well as problem areas in their development and ground developmental testing. The paper analyses pros and cons of using various versions of propulsion systems based on medium- and high-power electrical propulsion engines, the current status of their component development, as well as the technical feasibility of conducting developmental tests on the ground. Key words: electric propulsion engine, propulsion system, propulsion module, propellant storage system, power supply and control system, vacuum chamber, vacuum system.

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