General advanced upper stage of solid launch vehicle

• Main Authors: Sun Shupeng, Song Changzhe, Yan Haiping, Ding Bo, Wang Kun, Hu Changwei, Chi Xianbin, Wang Yufei, Gan Lin, Wang Bozhe, Liang Jiqiu, Duan Xiao, Wu Xiaomeng, Yan Yehui, Xie Yang, Xiao Renqin
• Format: Patent
• Language: Chinese; English
• Published: 10.08.2016
• Subjects: AIRCRAFT; AMMUNITION; AVIATION; BLASTING; CONTROLLING; COSMONAUTICS; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION; HEATING; LIGHTING; MECHANICAL ENGINEERING; PERFORMING OPERATIONS; PHYSICS; REGULATING; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES; TRANSPORTING; VEHICLES OR EQUIPMENT THEREFOR; WEAPONS

The invention provides a general advanced upper stage of a solid launch vehicle. The general advanced upper stage of the solid launch vehicle comprises an electrical part and a structural part. The electrical part is composed of an integrated electronic system single machine and a peripheral unit. The integrated electronic system single machine comprises a center control module, a signal collecting module, a measurement and control communication module, an attitude and orbit control module, a sequential control module and a power source and thermal control management module which are integrated and connected through a bus. The peripheral unit comprises an attitude control peripheral, a measurement and control communication peripheral, a power source peripheral, a propulsion peripheral and a thermal control peripheral. The structural part comprises a load mounting plate, an attitude control ring, a storage box, an instrument bay, a single machine mounting plate and a propulsion mounting plate, wherein the load