Rocket launching method and device, electronic equipment and computer readable storage medium

• Main Authors: LIU ZHAOBO, ZHANG SHIQIANG, GAO YUNYI, MU HONGBIN, YUE YONG, HUI XINGCHEN, WU WANTONG, ZHANG MINGGEN, CONG ENBO, XIAO XUE, GUAN HONGREN, LIU SIQI, BIAN XU, WANG ZHENGHAN, HE DINGZHOU, ZHANG GUOFENG, LIU WEI, LI HAOWEI, LIU JIAJIA, QI HUAN, WANG JINING, PU PENGYU, WU ZHOUHANG, XING ZHI, JIN XIN, ZHANG DONG, ZHANG WEN, ZHANG ZHONGZHOU, WANG HUI, JIA YINGHE, NIE SHU
• Format: Patent
• Language: Chinese; English
• Published: 16.08.2024
• Subjects: AMMUNITION; APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS; BLASTING; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION; HARPOON GUNS; HEATING; LAUNCHERS FOR ROCKETS OR TORPEDOES; LIGHTING; MECHANICAL ENGINEERING; WEAPONS

The invention discloses a rocket launching method and device, electronic equipment and a computer readable storage medium, and relates to the technical field of spaceflight and the technical field of rocket launching. The method comprises the steps that a task instruction corresponding to a rocket is received, and the task instruction indicates execution of a first task or a second task; under the condition that the task instruction indicates to execute the first task, a rocket fairing and a satellite are packaged into a star cover assembly in a vertical attitude, the star cover assembly is controlled to be in butt joint with the rocket on the launching ship to form a target assembly, and the target assembly is launched; and under the condition that the task instruction indicates to execute the second task, the rocket fairing, the satellite and the rocket are packaged into an integral assembly in a horizontal attitude, and the integral assembly is launched on the launching ship. The technical problem that in