Rocket combustible propellant filling platform and filling method

• Main Authors: SHEN BINGMEI, ZHANG JIAXIAN, CHAI DONGDONG, WANG LIJING, LIU ZHIHUA, LIU RUIMIN, WANG YONGCHAO, SONG JINGJING, GAO WANLI, CHEN YUZE
• Format: Patent
• Language: Chinese; English
• Published: 26.08.2022
• Subjects: BLASTING; HEATING; LIGHTING; MECHANICAL ENGINEERING; PIPE-LINE SYSTEMS; PIPE-LINES; STORING OF DISTRIBUTING GASES OR LIQUIDS; WEAPONS

The invention relates to the technical field of rocket low-temperature combustible propellant filling, and provides a rocket combustible propellant filling platform and a rocket combustible propellant filling method.The filling platform comprises a body of a box type structure; the fuel conveying unit is arranged in the body, the inlet end of the fuel conveying unit is suitable for being connected with an external fuel source, and the outlet end of the fuel conveying unit is suitable for being connected with a feeding port of a rocket; the nitrogen supply unit is arranged in the body, the inlet end of the nitrogen supply unit is suitable for being connected with an external nitrogen source, the outlet end of the nitrogen supply unit corresponds to the fuel conveying unit, and the nitrogen supply unit is suitable for providing replacement gas needed in the fuel adding process. According to the filling platform, the body is of a box-type structure, and the fuel conveying unit and the nitrogen supply unit are bo