Cockpit, avionics, performance, fq, hq and workload evaluationon l39 albatros for lift suitability
Başlık çevirisi mevcut değil.
- Tez No: 914203
- Danışmanlar: Belirtilmemiş.
- Tez Türü: Yüksek Lisans
- Konular: Belirtilmemiş.
- Anahtar Kelimeler: Belirtilmemiş.
- Yıl: 2022
- Dil: İngilizce
- Üniversite: International Test Pilot School
- Enstitü: Yurtdışı Enstitü
- Ana Bilim Dalı: Belirtilmemiş.
- Bilim Dalı: Belirtilmemiş.
- Sayfa Sayısı: 133
Özet
Calgary Ostrogoth Air Force (COAF) was looking to procure L39 Albatros aircrafts to train student pilots in LIFT mission for transition to 5 th generation aircrafts. COAF was searching for avionics upgraded L39s of International Test Pilots School (ITPS) for LIFT mission suitability to materialize its purpose. Test crew went through ground tests for cockpit ergonomics and avionics, inflight tests for mission related performance, flying qualities, handling qualities and workload. Although L39 had proven itself as a trainer and was promoted with some avionics coating, test team created a result effort without ignoring several key parameters that would act as a bridge between L39 and 5 th generation platforms. L39 was found to be incompetent as it didn't introduce symbology of cueing for air-to-air missile and gun attack with lack of ranging capability during offensive BFM. Even though L39's sufficient flying and handling qualities for offensive BFM and close formation flight, its handling qualities during maximum pulling on the brink of lift / thrust boundary and high workload introduced because of its avionics deficiencies in defensive BFM were assessed UNSATISFACTORY (CLASS II). HIGHLY DESIRABLE recommendations over findings were to be: 1. L39 should be equipped with a ranging device either as a sensor or bilateral data link between BFM players and forged with weapon employment cueing system, 2. L39's avionics should be modified to give aural alert for predefined fuel and altitude level, 3. COAF should consider impacts of poor handling qualities of L39 for pulling the stick at the thrust / lift boundary and compare its characteristics for transitioning to 5 th generation aircraft. Four more CLASS III deficiencies were presented into consideration. It would also be recommended to fulfill MIL-F-8785C remaining requirements that couldn't be conducted due to time constraints and lack of onboard test instruments. L39 evaluated UNSUITABLE for LIFT mission on grounds of a transition aircraft to 5 th generation platforms.
Özet (Çeviri)
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