Parameter

4.7.2.14 topology optimized lh2 tanks

Topology optimized LH2 tanks refer to the design of liquid hydrogen fuel tanks using topology optimization techniques which involve using algorithms to create complex internal structures that maximize storage capacity while minimizing weight and material usage resulting in more efficient and lightweight tanks for aerospace applications.

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
4.7 aircraft structures
4.7.1 aerospace materials & manufacturing
4.7.2 aircraft fuselage
4.7.2.1 fuselage smart structures
4.7.2.2 window-less fuselage
4.7.2.3 low drag fuselage
4.7.2.4 flow control (passive) on fuselage
4.7.2.5 excrescence
4.7.2.6 airframe as battery or ultra capacitor
4.7.2.7 twin fuselage
4.7.2.8 lifting fuselage
4.7.2.9 tube and wing optimization
4.7.2.10 fuselage structure as conductor
4.7.2.11 light/low mass paint/decals on fuselage
4.7.2.12 fuselage as antenna
4.7.2.13 droplet shaped fuselage
4.7.2.14 topology optimized lh2 tanks
4.7.3 aircraft wings
4.7.4 secondary structures

Scenario relevance

Number of parameter occurrence per scenario.

Input
Output
1
2
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