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TRM50™ 是一個用於測定壓力和推力曲線以及評估固體火箭推進劑燃燒參數的測量系統。 |
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應用 小型試驗通常用於火箭推進劑研發的最後階段，以經濟有效的方式提供接近全尺度火箭發動機的試驗結果。 |
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| 試驗火箭發動機測量到的壓力和推力曲線範例 | 根據火箭發動機測試測量結果評估燃燒率與壓力的關係 |
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合規
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| 帶 PC 的測量和控制單元 | |
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Sub-scale testing rocket motor TRM50™ is a measurement system designed for determination of pressure and thrust profiles and evaluation of combustion parameters of solid rocket propellants.
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APPLICATIONS The sub-scale testing is usually used in the final stages of research and development of the rocket propellants, providing results close to the full-scale rocket motor in a cost effective way. Compared to LTRM, the sub-scale testing rocket motor TRM 50 provides more complex results of ballistic experiments (maximum and mean pressure, pressure impulse, burning time, burning rate, specific impulse or temperature sensitivity coefficient) using variable chamber lengths and nozzle shapes. |
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| Example of pressure and thrust profiles measured in the Testing Rocket Motor |
Burning rate vs. pressure dependence evaluated from the Testing Rocket Motor measurements |
ADVANTAGES & FEATURES
- Combined pressure and thrust measurement
- Precise measurement and control unit with electric ignition
- Working pressure up to 500 bar
- Simple operation
- Set of testing motors and ABSW™ evaluation software included
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COMPLIANCE
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| Measurement and control unit with PC | |