Heping sounding rocket
The zn-3 sounding rocket is an important instrument used for the sounding of space science.
An calculating method for design parameter optimization of the propulsion system of the sounding rocket is given.
Space research activities are being aided through two sounding rocket launching stations sponsored by the United Nations.
This paper derives a set of differential equations which mustbe satisfied by the velocity elevation angle and velocity azimuth angle forsounding rocket. Under some approximation assumptions,the effects of thewind on the sounding rocket trajectory are analyzed.
