ポリカルポフ I-153 チャイカ

Polikarpov I-153

ソ連
役割 戦闘機
初飛行1937
構築3400+

ポリカルポフ I-153 チャイカ (ロシアのЧайка、「カモメ」)は1930年代後半のソビエト複葉戦闘機でした。格納式の下部構造を備えたI-15の高度なバージョンとして開発された、I-153は、モンゴルでのソビエトと日本の戦闘で戦い、第二次世界大戦の初期にはソビエトの主要な戦闘機タイプの1つでした。 3台のI-153がまだ飛んでいます。

ソース: ウィキペディアのポリカルポフ I-153
Polikarpov I-153 Chaika Walk Around
カメラマンロバートN.アボットジュニア
ローカライズ知りません
写真13
待って、ポリカールポフI-153を探して…

関連項目:

第二次世界大戦:電撃戦から原子爆弾までの決定的なビジュアルヒストリー(DK Definitive Visual Histories) - Amazon (アマゾン) 地図による第二次世界大戦の地図(地図によるDKの歴史地図) - Amazon (アマゾン)

Polikarpov's Biplane Fighters
ポリカルポフの複葉戦闘機

General Characteristics and Role

The Polikarpov I-153 Chaika (Russian for “Seagull”) was the final evolution in a line of highly maneuverable Soviet biplane fighters. It was developed in the late 1930s to combine the agility of its predecessor, the I-15, with increased speed and performance. Key features included a manually retractable landing gear to reduce drag, a gull-wing upper wing design (giving it the nickname Chaika), and improved armament. Although it was the fastest biplane ever to see operational service and performed well in early conflicts, it was rapidly made obsolete by the advent of faster monoplane fighters, such as those of the German Luftwaffe, by the time of the German invasion in 1941.

Property Typical Value (I-153 M-62)
役割 Fighter / Ground Attack Biplane
National Origin Soviet Union (USSR)
メーカー Polikarpov Design Bureau
First Flight August 1938
Production Total 3,437 aircraft built (1939–1941)
乗組員 1 (Pilot)
長さ 6.17 m (20 ft 3 in)
10.00 m (32 ft 10 in)
Empty Weight 1,452 kg (3,201 lb)
Loaded Weight 2,110 kg (4,652 lb)

Powerplant and Performance

  • Engine: One Shvetsov M-62 nine-cylinder, air-cooled radial engine.
  • Power Output: 746 kW (1,000 hp).
  • Maximum Speed (High Altitude): 444 km/h (276 mph) at 4,600 m (15,100 ft).
  • Maximum Speed (Sea Level): 366 km/h (227 mph).
  • Range: 470 km (290 mi) (internal fuel).
  • Service Ceiling: 10,700 m (35,100 ft).
  • Rate of Climb: 15 m/s (3,000 ft/min).
  • Key Feature: Retractable main undercarriage was manually operated by a hand crank in the cockpit.

武装

  • Guns (Standard): 4 x 7.62 mm ShKAS machine guns.
    • Cadence: High rate of fire (1,800 rounds per minute per gun), providing a high density of fire.
    • Location: Typically two synchronized guns in the fuselage and two in the lower wings.
  • Rockets: Provision for 8 x 82 mm RS-82 air-to-ground unguided rockets under the wings.
    • Note: This was one of the first aircraft widely equipped with air-to-ground rockets.
  • Bombs: Up to 200 kg (441 lb) of bombs (e.g., four 50 kg or eight 25 kg bombs).
  • Variants: Later production runs included versions armed with 12.7 mm UBS machine guns or 20 mm ShVAK cannons (I-153P).

再生 : 3714

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