题目内容

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

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

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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

The most important part to control the thrust of the liquid rocket engine is the ____.

A. Jet nozzle
B. Propellant feeding system
C. Propellant pump
D. Flow control valve

The thrust of solid rocket engine can be controlled by ____.

A. Control valve
B. Secondary injection technic
C. Different design of grain shape
D. Vectoring nozzle

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