Propellant shaking characteristic measurement flight test platform

The invention provides a flight test platform for measuring the shaking characteristic of a propellant. The platform comprises a test aircraft and a test control system, the test control system comprises an aircraft control system, a data measurement system and a test measurement and control system; the aircraft control system and the data measurement system are installed on the test aircraft. The test measurement and control system is arranged on the ground; the test aircraft comprises a test storage tank, and the test storage tank is filled with tested propellant liquid. According to the invention, an upper storage tank structure which is the same as that of a vertical take-off and landing liquid carrier rocket is used, a propellant shaking environment in a rocket reentry and return flight process is simulated, and force, heat, optics and other parameters of the propellant are measured. 本申请提供一种推进剂晃动特性测量飞行试验平台，该平台包括：试验飞行器和试验控制系统；所述试验控制系统包括飞行器控制系统、数据测量系统和试验测控系统；所述飞行器控制系统和所述数据测量系统安装于所述试验飞行器上；所述试验测控系统布置在地面；所述试验