產品介紹∣測試小型火箭發動機TRM 35
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測試小型火箭發動機TRM 35
TESTING SUB-SCALE ROCKET MOTOR TRM 35

【Ozm】火藥及危險易燃材料測試設備 含能材料燃燒速率檢測系列

測試小型火箭發動機TRM 35

簡介

TRM 35

The TRM 35 (TESTING SUB-SCALE ROCKET MOTOR) is designed for the measurement of the burning parameters of solid rocket propellants in a small scale rocket motor. During static testing the, TRM 35 measures and evaluates the pressure and thrust profiles of solid propellant in small testing rocket motors. The TRM 35‘s design and results are close to a real rocket motor. The TRM 35’s operation is simple and is capable of meeting a wide range of testing conditions.

我要諮詢

The TRM 35 (TESTING SUB-SCALE ROCKET MOTOR) is designed for the measurement of the burning parameters of solid rocket propellants in a small scale rocket motor. During static testing the, TRM 35 measures and evaluates the pressure and thrust profiles of solid propellant in small testing rocket motors. The TRM 35‘s design and results are close to a real rocket motor. The TRM 35’s operation is simple and is capable of meeting a wide range of testing conditions.

ADVANTAGES & FEATURES

  • Wider assessment of ballistic behavior of new or modified rocket propellant formulations
  • Pressure and thrust measurement with time
  • Customizable according to client’s needs
  • The results mimic that of a real rocket motortesting

The TRM 35, and sub-scale rocket motors in general, are a relatively new approved procedure in NATO STANAG standards. More individual shots are necessary to get the required parameters (e.g. burning rate, erosion influence, etc.) in the whole pressure range. The Subscale Rocket Motor is recommended as more universal supporting method. Measurement and evaluation by RMM is generally supplemented.

The TRM 35 (TESTING SUB-SCALE ROCKET MOTOR) is designed for the measurement of the burning parameters of solid rocket propellants in a small scale rocket motor. During static testing the, TRM 35 measures and evaluates the pressure and thrust profiles of solid propellant in small testing rocket motors. The TRM 35‘s design and results are close to a real rocket motor. The TRM 35’s operation is simple and is capable of meeting a wide range of testing conditions.

ADVANTAGES & FEATURES

  • Wider assessment of ballistic behavior of new or modified rocket propellant formulations
  • Pressure and thrust measurement with time
  • Customizable according to client’s needs
  • The results mimic that of a real rocket motortesting

The TRM 35, and sub-scale rocket motors in general, are a relatively new approved procedure in NATO STANAG standards. More individual shots are necessary to get the required parameters (e.g. burning rate, erosion influence, etc.) in the whole pressure range. The Subscale Rocket Motor is recommended as more universal supporting method. Measurement and evaluation by RMM is generally supplemented.