Parameter

4.6.4 non-combustion based engine integration

This refers to the integration of alternative propulsion systems, such as electric motors, hybrid-electric engines, or hydrogen fuel cells, that do not rely on traditional combustion processes, into aircraft designs. This integration offers potential benefits in terms of efficiency, zero or reduced greenhouse gas emissions, and noise reduction compared to conventional combustion engines.

Hierarchy

4 technological themes
4.1 active aircraft control
4.2 data transfer technologies
4.3 energy carriers
4.4 net zero technologies
4.5 operational technologies
4.6 aircraft propulsion
4.6.1 propulsor integration on airframe
4.6.2 converting shaft power to thrust
4.6.3 converting fuel to shaft power
4.6.4 non-combustion based engine integration
4.6.4.1 superconductive energy network
4.6.4.2 cryogenic electronics
4.6.4.3 integrated power electronics into e-motors
4.6.5 other propulsion technologies
4.7 aircraft structures

Scenario relevance

Number of parameter occurrence per scenario.

Input
Output
1
3
Optimising together
N/A
Stripping down
N/A
Tech for you
N/A
Mad max

Milestone Timehorizon

PESTEL categories

Current

Short term

Medium term

Long term

Little to many relations with other Milestones