“ducted rocket”可以造什么句，ducted rocket造句

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

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.

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

Numerical simulation and experimental study of deposition for ducted rockets

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