Parameter

4.6.1 propulsor integration on airframe

Propulsor integration on the airframe refers to the design and engineering process of integrating propulsion systems, such as engines, fans, or propellers, into the aircraft airframe. It involves optimizing the placement, mounting, and aerodynamic interaction of the propulsor with the airframe to minimize drag, maximize efficiency, and improve overall aircraft performance. Effective propulsor integration can reduce fuel consumption, emissions, and noise while also influencing the aircraft’s stability and control characteristics.

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
4.6.1.1 over-wing propulsors
4.6.1.2 forward fuselage mounted fans
4.6.1.3 tail cone thruster (e.g. starc-abl)
4.6.1.4 boundary layer ingestion rear end installation
4.6.1.5 in-wing distributed propulsion
4.6.1.6 retrofitting new propulsion systems
4.6.1.7 propulsive fuselage
4.6.2 converting shaft power to thrust
4.6.3 converting fuel to shaft power
4.6.4 non-combustion based engine integration
4.6.5 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