Propulsion System Component Considerations for NASA N3-X Turboelectric Distributed Propulsion System-Reference-Cited by-同舟云学术

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Propulsion System Component Considerations for NASA N3-X Turboelectric Distributed Propulsion System

Published:2012-10-22 Issue:2 Volume:5 Page:344-353
ISSN:1946-3901
Container-title:SAE International Journal of Aerospace
language:en
Short-container-title:SAE Int. J. Aerosp.

Author:

Armstrong Michael J.,Ross Christine A. H.,Blackwelder Mark J.,Rajashekara Kaushik

Publisher

SAE International

Subject

Aerospace Engineering

Cited by 32 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Fabrication and Test of a 400 kW-Class Fully Superconducting Synchronous Motor Using REBCO Tape for an Electric Propulsion System;IEEE Transactions on Applied Superconductivity;2024-08

2. A Review of Novel and Non-Conventional Propulsion Integrations for Next-Generation Aircraft;Designs;2024-02-20

3. A Review of Distributed Electric Aircraft Propulsion Architecture Progression;AIAA AVIATION 2023 Forum;2023-06-08

4. The Possibility of Using Superconducting Magnetic Energy Storage/Battery Hybrid Energy Storage Systems Instead of Generators as Backup Power Sources for Electric Aircraft;Sustainability;2023-01-17

5. A H‐type architecture for electric/hybrid‐electric aircraft propulsion systems;IET Electrical Systems in Transportation;2023-01-05

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