Kode Mata KuliahAE3202 / 4 SKS
Penyelenggara136 - Aerospace Engineering / FTMD
KategoriLecture
Bahasa IndonesiaEnglish
Nama Mata KuliahPropulsi Pesawat TerbangAircraft Propulsion
Bahan Kajian
  1. Review Termodinamika dan Termokimia
  2. Gaya dorong (thrust)
  3. Propeller
  4. Siklus ideal ramjet, turbojet, turboprop, turbofan
  5. Analisis siklus dengan rugi-rugi (losses), siklus aktual
  6. Komponen Jet (Inlet dan Nozzle, Compressor, Combustion Chamber, Turbine)
  7. Analisis performa roket propelan
  8. Propelan cair dan padat
  9. Propulsi hybrid dan electric
  1. Review of thermodyamics and thermochemistry
  2. Thrust
  3. Propeller
  4. Ramjet, Turbojet, Turboprop and turbofan ideal cycle
  5. Cycle analysis with losses, actual cycles
  6. Jet components (Inlet and Nozzle, Compressor, Combustion Chamber, Turbine)
  7. Performance analysis of rocket propellant
  8. Liquid and solid propellant
  9. Hybrid and electric propulsion
Capaian Pembelajaran Mata Kuliah (CPMK)
  1. Memahami prinsip dasar dan variable yang berpengaruh pada gaya dorong serta parameter prestasi mesin
  2. Memahami dan mampu melakukan analisis siklus termodinamika mesin propulsi ideal dan aktual
  3. Memahami dan mampu melakukan analisis turbomachinery/rotary component
  4. Memahami prinsip kerja inlet/nozzle dan burner
  5. Memahami prinsip kerja dan melakukan analisis sistem propulsi roket
  6. Memahami prinsip dasar dan mampu melakukan analisis sistem propulsi roket berbasis propelan cair dan padat
  7. Memahami konsep-konsep sistem propulsi non-konvensional (hybrid dan electric)
  1. Understand the basic principles and variables that affect thrust and engine performance parameters
  2. Understand and be able to perform thermodynamic cycle analysis of ideal and actual propulsion machines
  3. Understand and be able to perform turbomachinery/rotary component analysis
  4. Understanding the working principle of inlets/nozzles and burners
  5. Understand the working principle and conduct an analysis of the rocket propulsion system
  6. Understand the basic principles and be able to perform the analysis of rocket propulsion systems based on liquid and solid propellant
  7. Understand the concepts of non-conventional propulsion systems (hybrid and electric)
Metode PembelajaranTatap muka di kelas. Tutorial materi kuliahIn-person class, lecture tutorial
Modalitas PembelajaranLuring, sinkron, mandiriOffline, synchronous, independent
Jenis NilaiABCDE
Metode PenilaianUjian Tengah Semester Ujian Akhir Semester TugasMidterm Exam, Final Exam, Assignment
Catatan Tambahan