火箭發動機彈道測量系統

RMM （火箭發動機彈道測量系統 ）是為測量安裝在試驗台上不同類型火箭發動機的推力和壓力曲線而設計的。

RMM 是研究和開發不同類型的客製化和使用者特定火箭發動機、彈藥筒驅動裝置和推進劑驅動裝置的理想解決方案，用於製造和在役監控中的品質控制。

 

應用 火箭發動機彈道測量系統（RMM）用於測量安裝在支架上的火箭發動機燃燒不同類型固體推進劑時火箭發動機腔內的 壓力和火箭發動機隨時間變化的推力（威力）。
在載台上測量兩種不同火箭發動機的壓力和推力曲線範例

優勢和特點

• 透過應變片感測器對壓力和推力進行動態測量，記錄時間長，並結合精確定義的電子點火裝置。
• 可選溫度、光或動態壓電測量功能。
• 先進的數據蒐集和評估軟體，操作簡單。
• 提供客製化服務，以便將客戶的發動機和應用，可與 RMM 設定完美搭配。
• 系統不包括火箭發動機裝置。
   

帶 PC 的測量和控制單元

The RMM™ (Rocket Motor Ballistic Measurement) is a system designed for the measurement of thrust and pressure profiles of different types of rocket motors mounted on a test stand. 

The RMM is an ideal solution for the research and development of different types of customized and user-specific rocket motors, cartridge-actuated devices and propellantactuated devices, for their quality control in manufacture and in-service surveillance.
 

APPLICATIONS  Rocket Motor Ballistic Measurement (RMM) is used for the measuring of pressure inside rocket motor chamber and thrust (force) of rocket motor with time during burning different types of solid propellant in rocket motors mounted on stand.
Examples of measured pressure and thrust profiles of two different rocket motors on a stand

ADVANTAGES & FEATURES

• Dynamic measurement of pressure and thrust by strain-gauge  transducers with long record times,
  combined with precisely  defined electrical ignition
• Optional temperature, light or dynamic piezoelectric measurement available
• Sophisticated data acquisition and evaluation software with simple operation
• OZM Research provides necessary tailoring  for fitting the customer’s motors and applications  to the RMM setup
• Rocket motor IS NOT INCLUDED
   

Measurement and control unit with PC