The Kamov Ka-26 (NATO reporting name Hoodlum) is a Soviet light utility helicopter with co-axial rotors. The Ka-26 entered production in 1969 and 816 were built. A variant with a single …

卡-26直升机（英文：Kamov Ka-26）是苏联研制的农业直升机。 卡-26直升机采用两副共轴反转的三片桨叶旋翼系统。 卡-26直升机1970年投入使用，该机寿命与经济性高，可快速改装，能适用于多种用途，比如喷洒农药和施化肥等。

The Kamov Ka-26, which has the NATO codename Hoodlum, was announced in January 1964 as a light commercial helicopter with twin-turbine powerplant and a design making it easily convertible to meet the requirements of several roles. The primary task envisaged for the Ka-26, however, was agricultural.

The uniquely configured Ka26 features two counter rotating main propellers, a Kamov characteristic that negates the need for an anti torque tail rotor. Other features include the two podded radial piston engines mounted either side of the fuselage, and the removable and exchangeable rear fuselage.

2012年11月21日 · Ka-26是设计局制造的多用途直升机并以此命名。 卡莫夫（根据北约编纂：Hoodlum - “流氓”）。 在乌兰乌德的飞机制造厂以及 航空 工厂位于 Kumertau 市。 该型直升机共生产816架，其中257架出口到14个国家。

The Kamov Ka-26 (NATO reporting name Hoodlum) is a Soviet light utility helicopter with co-axial rotors. The Ka-26 entered production in 1969. 816 have been built. A variant with a single engine was the Ka-126. A turboshaft-powered version is the Ka …

The Kamov Ka-26 is a twin-engined light utility helicopter with coaxial rotors developed by the Soviet Design Bureau OKB Kamov (OKB-2), today Kamov JSC, Russia. The Ka-26 can be operated with or without the interchangeable mission pod (cabin). The main roles are agricultural service, air ambulance, cargo and passenger transport and firefighting.

The Ka-26 (NATO name “Hoodlum”) is a light utility helicopter created by the Kamov design bureau. The Ka-26 first took flight in 1965 and was officially introduced in 1969. The Ka-26 …

This document provides a history and description of Kamov's naval helicopters -- Ka-15, Ka-25, and Ka-27, plus their derivatives -- as well as the Ka-26 light civil utility helicopter, and its derivatives.

Kamov Ka-26 holds five aviation world records, among them is climb record – 5330 meters (for helicopters with take-off weight 1750 – 3000 kg) and rate of climb record – it gained altitude of 3000 meters in 51 seconds.