Wargaming.net 위키에 오신 것을 환영합니다!
변수

Gloster P.228

이동: 둘러보기, 검색





P.228

Icon
Totals
3540000 가격
900 내구도
11030 kg중량
601.3 공격력
Speed
2135.8 대기 속도
900 km/h해수면 최고 속도
900 km/h최적 고도 최고 속도
2500 m최적 고도
1100 km/h최고 급강하 속도
111.7 m/s상승률
250 km/h실속 속도
671 km/h최적 대기 속도
Mobility
77.8 조종성
15.4 초평균 360도 선회 시간
70 °/s횡전율
880.1 기동성
IX
Gloster P.228
3540000
2인승 야간 전투기 계획으로 설계단계에서 개발이 중지되었다.

엔진

엔진

단계 엔진 엔진 출력, hp / 추력 종류 중량, kg 가격,
IX AS Sapphire Sa.5 3402 제트 2680 150000
IX MV Sapphire Sa.1 3175 제트 2670 140000
X AS Sapphire Sa.5R 4173 제트 2700 180000
X NAME_MODULE_SA-5R_SPEC_TOP_GLOSTER-P-228_1 4173 제트 2700 180000
기체

기체

단계 기체 내구도 중량, kg 가격,
IX Gloster P.28 900 8000 175000
엔진 덮개 장착 무기

엔진 덮개 장착 무기

단계 기관총 구경 포구 속도, m/s 공격력 발사 속도, rounds/min 중량, kg 가격,
VIII 20 mm Hispano Mk.V* (엔) 20 1760 130 420 90 54000
X WEAPON_NAME_G30MM-ADEN-F_SPEC_TOP_GLOSTER-P-228_1 30 1520 330 300 120 85000
외부 장착 무기

외부 장착 무기

단계 로켓 피해 반경, m 공격력 중량, kg 가격,
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