Parameter

3.1.2.5 gas turbine systems

Gas turbine systems are the primary thermal propulsion units of modern aircraft that must be adapted to combust alternative fuels such as hydrogen or sustainable aviation fuel. These adaptations allow for significant direct carbon reductions without fully redesigning the airframe. Challenges in developing these modified systems lie in managing high combustion temperatures, preventing flashback when burning hydrogen, and minimizing nitrogen oxide emissions.

Hierarchy

3 product service systems
3.1 aircraft product systems
3.1.1 components
3.1.2 Aircraft systems
3.1.2.1 auxiliary systems
3.1.2.2 battery electric powertrain systems
3.1.2.3 cabin systems
3.1.2.4 flight control systems
3.1.2.5 gas turbine systems
3.1.2.6 hybrid powertrain systems
3.1.2.7 hydrogen powertrain systems
3.1.2.8 landing gear systems
3.1.2.9 novel fuselage
3.1.2.10 novel wings
3.1.2.11 SAF powertrain systems
3.2 development supporting services
3.3 flight supporting service systems

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