Parameter

4.6.1.1.1 slipper-mount over-wing nacelle

is an aircraft engine installation where the engine nacelle is mounted directly on top of the wing in a “slipper” (pylon-less) configuration, sliding or bonded along the upper wing surface, and often configured to blow exhaust or jet flow over the wing to generate additional lift.
This configuration can reduce ground-clearance issues, ease integration of high-bypass engines, and provide noise shielding because the wing blocks fan and jet noise from the ground.

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
4.6.1.1.1 slipper-mount over-wing nacelle
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
1
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