男女牲交过程视频播放免费LM-3A is a 3-stage launch vehicle developed on the basis of LM-3 and LM- 2C. Its third stage is powered by cryogenic propellants --- liquid hydrogen and liquid oxygen. It is mainly usec for launching spacecraft with GTO mission. Its launch capability for GTO mission is 2,600 kg. The fairing static envelope is 3m in diameter.