The paper presents a modified method of solid propellant rocket motor design based on results of unguided rocket trajectory solution being consequently used for the rocket motor parameters determination for given tactical and technical requirements and s
The paper presents a modified method of solid propellant rocket motor design based on results of unguided rocket trajectory solution being consequently used for the rocket motor parameters determination for given tactical and technical requirements and s (en)
Raketový motor s dělenou náplní tuhé pohonné hmoty (cs)