题目内容

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

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

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____ 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

When bidirectional swinging nozzle’s two opposite nozzles swing in the same direction, it could controls the ____ motion of the rocket.

A. Yaw
B. Pitch
C. Rolling
D. Sideslip

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