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Gloster P.228

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P.228

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Totals
3540000 Prix
900 Capacité de survie
11030 kgPoids
601.3 Dégâts
Speed
2135.8 Vitesse
900 km/hVitesse max. au ras du sol
900 km/hVitesse max. à altitude idéale
2500 mAltitude optimale
1100 km/hVitesse en piqué
111.7 m/sTaux de montée
250 km/hVitesse de décrochage
671 km/hVitesse optimale
Mobility
77.8 Contrôlabilité
15.4 sTemps moyen de rotation 360°
70 °/sTaux de roulis
880.1 Maniabilité
IX
Gloster P.228
3540000
Projet pour un nouveau chasseur nocturne biplace. Le développement a été interrompu lors de la phase de conception.

Moteur

Moteur

Rang Moteur Puissance du moteur, ch / Poussée Type Poids, kg Prix,
IX AS Sapphire Sa.5 3402 avion à réaction 2680 150000
IX MV Sapphire Sa.1 3175 avion à réaction 2670 140000
X AS Sapphire Sa.5R 4173 avion à réaction 2700 180000
X NAME_MODULE_SA-5R_SPEC_TOP_GLOSTER-P-228_1 4173 avion à réaction 2700 180000
Cellule d'avion

Cellule d'avion

Rang Cellule d'avion Capacité de survie Poids, kg Prix,
IX Gloster P.28 900 8000 175000
Armement du carénage

Armement du carénage

Rang Mitrailleuse Calibre Vitesse initiale, m/s Dégâts Cadence de tir, coups/min Poids, kg Prix,
VIII 20 mm Hispano Mk.V* (C) 20 1760 130 420 90 54000
X WEAPON_NAME_G30MM-ADEN-F_SPEC_TOP_GLOSTER-P-228_1 30 1520 330 300 120 85000
Armement extérieur

Armement extérieur

Rang Roquettes Rayon des dégâts, m Dégâts Poids, kg Prix,
VIII WEAPON_NAME_RP-3-GP_SPEC_TOP_GLOSTER-P-228_1 35 1500 37 800


Compatible Equipment

Compatible Consumables


Informations Historiques

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 et Liens Externes

de:Plane:Gloster-p-228