A launch vehicle heat shield aerodynamic load simulation test device
By designing a pneumatic load simulation test device that includes a cylindrical section, connecting flanges, and a measurement and control system, the problem of accurately evaluating the load-bearing performance of the heat-resistant skirt in the existing technology has been solved, realizing low-cost, short-cycle simulation tests and improving the accuracy and efficiency of the test.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- BEIJING LANDSPACETECH CO LTD
- Filing Date
- 2026-05-21
- Publication Date
- 2026-07-17
AI Technical Summary
The existing technology lacks a low-cost, short-cycle test device that can effectively simulate the thermal protection skirt of a launch vehicle under the coupled action of aerodynamic and thermal loads, making it difficult to accurately evaluate the overall structural load-bearing response and failure mode of the thermal protection skirt.
A pneumatic load simulation test device was designed, comprising a first cylindrical section, a connecting flange, a mounting plate, and a measurement and control system. The device simulates pneumatic loads through a pressurization interface, a pressurization pipeline, and a pressure sensor. Combined with sealant and a camera to monitor the deformation of the heat-resistant skirt, the device simulates the actual load-bearing performance of the heat-resistant skirt.
It reduces testing costs and implementation difficulty, shortens the testing cycle, and can accurately simulate the load-bearing performance of the heat-resistant skirt under the coupled action of aerodynamic and thermal loads on the ground.
Smart Images

Figure CN122409362A_ABST