Parameter

4.6.2.2 open rotor

An open rotor is a type of propulsion system that features a rotor or fan without a traditional duct or shroud. Unlike ducted fans, open rotors have exposed blades that operate in free air, generating thrust through the acceleration of air rearward.
Open rotors are designed to be more efficient at high speeds and can offer advantages such as, reduced weight and complexity compared to ducted fans, improved thrust-to-weight ratio, increased efficiency at high speeds, potential for reduced fuel consumption and emissions.
However, open rotors can also produce more noise and may be more susceptible to foreign object damage (FOD) due to the exposed blades.

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
4.6.2.2 open rotor
4.6.2.2.1 installation on wing
4.6.2.2.2 installation on rear end
4.6.2.2.3 novel swirl recovery
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
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