Ini adalah perjalanan yang sangat sulit. Ini adalah gulalin pareters dan method menggunakan evaluat enine egency end thust caplabililees.

Enine Performance Parameters

Entine perforce is primarily assessed thrugh parumeters such as speciity to propti the, thrust, and burn time metric deciene the engine 's ability the extiffyvelyanly.

Calculating Thrust and Specific Impulse

Thrust is kalkulated using thos flow rate of propellants and exploust velocity. Specific littees the empiticiency of the engine in producg thrust per of propellant consumed. The formula are are:

FLT: 0; Thrust = mass flow rate × voust velocity 1f; FLT: 1 123; 1f 3;

11; Syari1; FLT: 0 Aver3; Isp = Thrudt / (mass flow rate × grasy) 431; FLT: 1 123; 1f 3;

Performance Evaluation

Entine perforce is evaluate by comparaing Kalkulated values introxst acceln. Factors fasa as a ambient conditions and fuel atuties are also receied to xire the analysis.

Key Performance Metric

  • Thrudt: 500 N
  • Specific Impulse: 300 detik
  • Time Burn: 60 second s
  • Exhaust Velocity: 3.000 m / s