Thermal Design and Experimental Verification of a Three-Dimensional-Printed Resistojet
Author:
Affiliation:
1. Muroran Institute of Technology, Muroran, Hokkaido 050-8585, Japan
2. Japan Aerospace Exploration Agency, Tsukuba, Ibaraki 305-8505, Japan
3. NTT Data XAM Technologies Corporation, Minoo, Osaka 562-0035, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38187
Reference21 articles.
1. Electric propulsion for satellites and spacecraft: established technologies and novel approaches
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3. 3-KW concentric tubular resistojet performance.
4. Spacecraft Electric Propulsion-An Overview
5. DohertyM.MeyerM.MotilS.GintyC. “Cryogenic Propellant Storage and Transfer Technology Maturation: Establishing a Foundation for a Technology Demonstration Mission,” NASA TM-2014-218092, 2014.
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