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Gloster P.228

Atla: kullan, ara


3540000 Fiyat
900 Beka
11030 kgAğırlık
601.3 Hasar
2135.8 Hava Hızı
900 km/sa.Deniz Seviyesinde Azami Hız
900 km/sa.En İyi İrtifada Azami Hız
2500 mOptimum İrtifa
1100 km/sa.Maksimum Pike Hızı
111.7 m/sn.Tırmanma Hızı
250 km/sa.Stall Hızı
671 km/sa.Optimum Hava Hızı
77.8 Kontrol edilebilirlik
15.4 sn.Ortalama 360 Derece Dönüş Süresi
70 °/sn.Yatma Hızı
880.1 Manevra Kabiliyeti
Gloster P.228
Yeni bir iki-kişilik gece avcısı projesi. Tasarım dönemi sırasında geliştirmeye son verildi.



Seviye Motor Motor Gücü, bg / İtme Kuvveti Tip Ağırlık, kg Fiyat,
IX AS Sapphire Sa.5 3402 jet 2680 150000
IX MV Sapphire Sa.1 3175 jet 2670 140000
X AS Sapphire Sa.5R 4173 jet 2700 180000
X NAME_MODULE_SA-5R_SPEC_TOP_GLOSTER-P-228_1 4173 jet 2700 180000


Seviye Gövde Beka Ağırlık, kg Fiyat,
IX Gloster P.28 900 8000 175000
Kaporta-üstü silah

Kaporta-üstü silah

Seviye Makineli tüfek Kalibre Namlu Çıkış Hızı, m/sn. Hasar Ateş Hızı, mermi/dakika Ağırlık, kg Fiyat,
VIII 20 mm Hispano Mk.V* (M) 20 1760 130 420 90 54000
X WEAPON_NAME_G30MM-ADEN-F_SPEC_TOP_GLOSTER-P-228_1 30 1520 330 300 120 85000
Dıştan takma silah

Dıştan takma silah

Seviye Roketler Hasar Yarıçapı, m Hasar Ağırlık, kg Fiyat,

Compatible Equipment

Compatible Consumables

Historical Info

In the aftermath of the Second World War, Britain identified a threat posed by the jet-powered strategic bomber and atomic weaponry and thus placed a great emphasis on developing aerial supremacy through continuing to advance its fighter technology, even following the end of conflict. In early 1947, the British Air Ministry released one request for proposals to the country's aviation industry.

The specification "F.44/46" called for a two-seat night fighter, that would intercept enemy aircraft at heights of up to at least 40,000 feet. It would also have to reach a maximum speed of no less than 525 kts at this height, be able to perform rapid ascents and attain an altitude of 45,000 feet within ten minutes of engine ignition.

The Gloster company submitted the "P.228" design in response to the requests. The P.228 night fighter was essentially an evolved derivative of Gloster's classic Meteor day fighter. The Gloster P.228 had an orthodox tail and fin and four 30mm cannons in the lower fuselage. A Sea level rate of climb 10,700 fl/min (3,261m/min) with 11.25 minutes needed to reach 45,000ft was planned for this aircraft. This project was abandoned in fovour of more advanced delta wing project P.234 and P.238, which resulted at the end in the Gloster Javelin.

Historical Gallery

Sources and External Links