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Aviation

Airplane

Project

Passenger

Liner

Model

Fuselage

Horizontal stabilizer

Rocket

Distance

Meter

Diameter

Cabin

Technological

Problem

Thermodynamics

Aerodynamics

Per cent

Efficiency

Extreme

Temperature

Cryogenic

Supersonic

Hypersonic

Paris

Tokyo

Plane

Hours

Reliable

Combined

Engine

Heat-insulating

Extreme

Generate

Generation

In general

Require

Fuel

Liquid

Hydrogen

Surface

Vaporize

Inject

Combustion

Chamber

Percentage

Amount

Announce

Combine

Combined with

Combustion

Complicated

Conventional

Currently

Disadvantage

Measure

Noise

Overall

Overcome

Resistance

Stress

Efficiency

e.g.(for example)

expect

friction

fuel

heat

inject

mainly

structure

substitute

vaporize

velocity

apart from

way out