小型試驗火箭發動機系統

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。

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。
與LTRM 相比，小型測試火箭發動機系統TRM 50 ，利用可變的腔室長度和噴嘴形狀提供了更複雜的彈道實驗結果
（最大和平均壓力、壓力脈衝、燃燒時間、燃燒速率、比衝量或溫度靈敏係數）。

合規

• STANAG 4672
• STANAG 4673

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.

 APPLICATIONS  

The sub-scale testing is usually used in the final stages of research and development of the rocketpropellants,
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 nozzleshapes.

 COMPLIANCE

• STANAG 4672
• STANAG 4673