SPECIFICATIONS
 

Wingspan: 10.97m , length: 8.59m, height: unknown, empty mass : 3,111 kg,
start mass:
4,631kg,
engine:
1 x Klimov VK-1 turbojet, 2,700kg
max speed:
1,105kn/h
initial climb: unknown.,
ceiling:
15,000m, range w/max.fuel: 1,000km,
Crew:
1,
Armament:2x23mm cannons NS-23 1
x37mm cannon N-37

 

 

S.A.Lavochkin La-176 1948
Russia

The La-176 illustrated the rapid pace of jet fighter development during the late 1940s. The aircraft featured highly swept wing and tail surfaces mated to a relatively clean fuselage. The fuselage housed a single turbojet engine fed by a large nose intake similar to that of the F-86 Sabre, MiG-15 and many other early jets. It became the first Soviet (World??) fighter to demonstrate sustained horizontal supersonic flight (after shallow dive acceleration). This happened December 26, 1948 with pilot I.E.Fedorov on controls. Later speed M=1.02 was demonstrated by O.V.Sokolovskij in shallow dive.

ラボーチキン設計局で設計されたジェット戦闘機です。MiG15やF-86Fのように機首のインテークから空気を吸入してストレートにエンジンに導入するという当時のコンベンショナルな設計と言えるでしょう。また超音速を達成したソ連初の航空機でもあります。軽いダイブのあと水平飛行でマッハ1.05の記録を打ち立てました。ちなみに1948年12月26日のことです。