Difference between revisions of "Electric Aircraft Propulsion Architectures"

From MIT Technology Roadmapping
Jump to navigation Jump to search
(include the types in gif format)
Line 5: Line 5:
The unique identifier for this roadmap is:  
The unique identifier for this roadmap is:  
* '''3EAPA - Electric Aircraft Propulsion Architectures'''
* '''3EAPA - Electric Aircraft Propulsion Architectures'''
This indicates that we are dealing with a “level 3” roadmap at the subsystem level, where "level 1" would indicate a market level roadmap (airline industry), “level 2” would indicate a product level roadmap (aircraft) and “level 4” would indicate an individual technology roadmap (propulsion subsystem components). We are considering this roadmap of propulsion architectures as "level 3" because it is being developed specifically for aircraft applications (only one relevant "level 2" roadmap).
This indicates that we are dealing with a “level 3” roadmap at the subsystem level, where "level 1" would indicate a market level roadmap (airline industry), “level 2” would indicate a product level roadmap (aircraft) and “level 4” would indicate an individual technology roadmap (propulsion subsystem components). We are considering this roadmap of propulsion architectures as "level 3" because it is being developed specifically for commercial aircraft applications (only one relevant "level 2" roadmap).


==Roadmap Overview==
==Roadmap Overview==

Revision as of 18:10, 10 October 2021

Team members: Josh Weisburg, Scarlett Koller, Jennifer Pandolf

Technology Roadmap Sections and Deliverables

The unique identifier for this roadmap is:

  • 3EAPA - Electric Aircraft Propulsion Architectures

This indicates that we are dealing with a “level 3” roadmap at the subsystem level, where "level 1" would indicate a market level roadmap (airline industry), “level 2” would indicate a product level roadmap (aircraft) and “level 4” would indicate an individual technology roadmap (propulsion subsystem components). We are considering this roadmap of propulsion architectures as "level 3" because it is being developed specifically for commercial aircraft applications (only one relevant "level 2" roadmap).

Roadmap Overview

Electric Propulsion.JPG

https://ntrs.nasa.gov/api/citations/20160009274/downloads/20160009274.pdf

All-electric.gif Parallel-hybrid.gif Series-hybrid.gif Turbo-electric.gif

Design Structure Matrix (DSM) Allocation

Roadmap Model using OPM

Figures of Merit

EASA FOM PowervsTime.JPG

Alignment with Company Strategic Drivers

TBD - To be developed

Positioning of Company vs. Competition

TBD

Technical Model

TBD

Financial Model

TBD

Key Publications, Presentations and Patents

TBD

Technology Strategy Statement

TBD