用ducted rocket造句子，“ducted rocket”造句

Study on theoretical performance of solid ducted rocket based on thermodynamic calculation

The effects of TMOs and their mixtures on the burning rate and the pressure exponent of the aluminum magnesium fuel rich propellant for unchoked ducted rocket are investigated.

The characterization of the combustion properties of the aluminum? magnesium fuel? rich propellant for unchoked ducted rocket was studied.

Numerical simulation and experimental study of deposition for ducted rockets

Analysis of flux-adjustable and ramjet-nozzle-adjustable solid ducted rocket