题目内容

The thrust generated by propellers of turboprop engines took ____ of the total thrust.

A. 10%
B. 50%
C. 75%
D. 90%

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The compression of air is finished in the ____ of ramjet.

A. Intake ducts
B. Compressor
C. Turbines
D. Nozzle

The "Helios" UAV of the United States have ____ propellers.

A. 10
B. 12
C. 14
D. 16

The thrust-to-weight ratio of rocket engines could reaches ____.

A. 30-40
B. 50-70
C. 80-120
D. 100-150

____ is a kind of the chemical energy rocket engines.

A. Solar energy rocket engine
B. Electric energy rocket engine
C. Solid-liquid hybrid rocket engine
D. Nuclear energy rocket engine

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