Sistem Patent
Utility Model Application

Tek Yönlü Turbo Jet Hipersonik Motor

Invention Abstract

FÜZE VEYA İNSANSIZ HAVA ARAÇLARI İÇİN KULLANILAN HİPERSONİK MOTOR İLE ALAKALI OLUP ÖZELLİĞİ TEK YÖN TURBO JET MOTOR İLE HİPERSONİK MOTORUN BİR ARADA OLMASIDIR. TR 2022 008277 U5

IPC Classes
F02K 7/16
Parties
Applicant
Barış Işık
Inventor
Barış Işık

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