TESTING SUB-SCALE ROCKET MOTOR TRM 35

TESTING SUB-SCALE ROCKET MOTOR <br />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.

 

APPLICATION

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.

 

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

order of the questions about TESTING SUB-SCALE ROCKET MOTOR TRM 35

OZM Explosives testing instruments Burning rate tests TESTING SUB-SCALE ROCKET MOTOR TRM 35
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