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Varianten

Gloster P.228

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P.228

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Totals
3540000 Kosten
900 Überlebensfähigkeit
11030 kgGewicht
601.3 Schaden
Speed
2135.8 Fluggeschwindigkeit
900 km/hV(max.) auf Meeresspiegel
900 km/hV(max.) bei opt. Flughöhe
2500 mOptimale Höhe
1100 km/hMax. Sturzfluggeschw.
111.7 m/Sek.Steigrate
250 km/hGeschwindigkeit Strömungsabriss
671 km/hOptimale Fluggeschwindigkeit
Mobility
77.8 Steuerbarkeit
15.4 Sek.Mittlere Zeit für 360-Grad-Kurve
70 °/Sek.Rollrate
880.1 Manövrierbarkeit
IX
Gloster P.228
3540000
Entwurf eines zweisitzigen Nachtjägers. Entwicklung wurde früh aufgegeben.

Motor

Motor

Stufe Motor Motorleistung, PS / Schub Typ Gewicht, kg Kosten,
IX AS Sapphire Sa.5 3402 Strahltriebwerk 2680 150000
IX MV Sapphire Sa.1 3175 Strahltriebwerk 2670 140000
X AS Sapphire Sa.5R 4173 Strahltriebwerk 2700 180000
X NAME_MODULE_SA-5R_SPEC_TOP_GLOSTER-P-228_1 4173 Strahltriebwerk 2700 180000
Flugwerk

Flugwerk

Stufe Flugwerk Überlebensfähigkeit Gewicht, kg Kosten,
IX Gloster P.28 900 8000 175000
Haubenmontierte Waffe

Haubenmontierte Waffe

Stufe Maschinengewehr Kaliber Mündungsgeschwindigkeit, m/Sek. Schaden Feuerrate, Schuss/Min. Gewicht, kg Kosten,
VIII 20 mm Hispano Mk.V* (H) 20 1760 130 420 90 54000
X WEAPON_NAME_G30MM-ADEN-F_SPEC_TOP_GLOSTER-P-228_1 30 1520 330 300 120 85000
Außenwaffe

Außenwaffe

Stufe Raketen Schadensradius, m Schaden Gewicht, kg Kosten,
VIII WEAPON_NAME_RP-3-GP_SPEC_TOP_GLOSTER-P-228_1 35 1500 37 800


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