Parameter

4.6.2.1.1 short nacelle

A short nacelle refers to a compact engine casing or housing designed to be shorter in length than a conventional nacelle. Short nacelles are often used in aircraft where space is limited or where minimizing drag is important, such as in advanced transport aircraft, business jets, or military aircraft. The reduced length can help lower installation drag and improve aerodynamic integration, which may increase efficiency and performance.
However, short nacelles can also create design challenges, including noise control, thermal management, and maintaining sufficient accessibility for maintenance,

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
4.6.2.1 advanced nacelle
4.6.2.1.1 short nacelle
4.6.2.1.2 laminar nacelle
4.6.2.1.3 ducted fan
4.6.2.2 open rotor
4.6.2.3 rim-driven fan
4.6.2.4 tip-drive fan
4.6.2.5 variable pitch fan blades
4.6.2.6 multi-engine single propulsor
4.6.2.7 composite fan blades & containment
4.6.2.8 gas turbine technology
4.6.2.9 composite cycle engine
4.6.2.10 high speed electric propulsion
4.6.2.11 electric boosting of combustion engines
4.6.2.12 direct drive technology
4.6.2.13 gas turbine + fuel cell (sofc)
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