To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Nakajima Ki-34

From Wikipedia, the free encyclopedia

Ki-34
Nakajima AT-2, civil version of the Ki-34
Role Civil airliner/Light military transport aircraft
Manufacturer Nakajima Aircraft Company
First flight 12 September 1936
Introduction 1937
Primary users IJA Air Force
IJN Air Service
Dai Nippon Koku KK
Manchukuo National Airways
Number built 351

The Nakajima Ki-34 was a Japanese light transport of World War II. It was a twin-engine, low-wing monoplane; the undercarriage was of tailwheel type with retractable main units. During the Pacific War, the Allies assigned the type the reporting name Thora.

YouTube Encyclopedic

  • 1/4
    Views:
    9 237
    82 164
    3 685
    14 258
  • Messerschmitt Bf 110: "Identification Of Aircraft: Messerschmitt Me-110" ~ 1942 US Army
  • GEE BEE R2 GIANT SCALE RC RACER PLANE FLIGHT DEMONSTRATION / Mega RC Airshow Göttingen 2015
  • Lavochkin La-7 Soviet WW2 fighter
  • Yakovlev Yak-3 Soviet WW2 fighter

Transcription

Design and development

The Ki-34 was originally designed as a civil transport. Nakajima Aircraft Company, which had the license-production rights to the Douglas DC-2, began design work in 1935 on a smaller twin engine airliner for routes which did not have the capacity to justify use of the larger DC-2. The initial design was designated AT-1, and after numerous design iterations, flew as a prototype designated AT-2 on 12 September 1936.[1] The design was all metal, except for the flight control surfaces, which were plywood. The wings used a multi-cell cantilever design. The prototype was fitted with 432 kW (580 hp) Nakajima Kotobuki 2-1 radial engines with fixed pitch wooden propellers, which were replaced in production models with Kotobuki-41 529 kW (710 hp) nine-cylinder radial engines, with variable pitch metal propellers.

Operational history

Civil use (AT-2)

A total of 32 AT-2s were produced for Imperial Japanese Airways (Dai Nippon Koku KK) and Manchukuo National Airways,[2] operating on scheduled routes between Tokyo and Xinjing, Tokyo and Tianjin, and within Manchukuo. These aircraft remained in operational service until the surrender of Japan in August 1945.

Military history (Ki-34 and L1N1)

Airborne Scene from "Kato hayabusa sento-tai [Colonel Kato's Falcon Squadron] 

With a high demand for increased military transport capability after the start of the Second Sino-Japanese War in 1937, the Imperial Japanese Army adapted the AT-2 design for military use by fitting with more powerful Nakajima Ha-1b radial engines and re-designating the aircraft as the Army Type 97 Transport and Ki-34. The initial 19 aircraft were produced by Nakajima Aircraft, and another 299 aircraft were subsequently produced by the Army-affiliated Tachikawa Hikoki K.K. The final airframe was delivered in 1942.

In operational service, the Ki-34 was used as a utility aircraft for liaison and communications duties, and for paratrooper training and Special Forces operations.

At a later date, some aircraft were transferred to the Imperial Japanese Navy, where they were known as the Navy Type AT-2 Transport or Nakajima L1N1. Several were also transferred to the air force of the Japanese puppet state of China-Nanjing in 1942.

Operators

Military operators

China-Nanjing
 Japan

Civil operators

 Japan
 Manchukuo
 Mongolia

Specifications (Ki-34)

Data from Japanese Aircraft of the Pacific War,[2] Warbirds Resource Group[3]

General characteristics

  • Crew: 3
  • Capacity: 8 pax
  • Length: 15.3 m (50 ft 2 in)
  • Wingspan: 19.916 m (65 ft 4 in)
  • Height: 4.15 m (13 ft 7 in)
  • Wing area: 49.2 m2 (530 sq ft)
  • Empty weight: 3,500 kg (7,716 lb)
  • Gross weight: 5,250 kg (11,574 lb)
  • Powerplant: 2 × Nakajima Kotobuki 41 or Nakajima Ha-1 9-cylinder air-cooled radial piston engines, 530 kW (710 hp) each for take-off
582 kW (780 hp) at 2,800 m (9,200 ft)
  • Propellers: 2-bladed variable-pitch propellers

Performance

  • Maximum speed: 360 km/h (220 mph, 190 kn) at 3,360 m (11,000 ft)
  • Cruise speed: 310 km/h (190 mph, 170 kn)
  • Range: 1,200 km (750 mi, 650 nmi)
  • Service ceiling: 7,000 m (23,000 ft)
  • Time to altitude: 3,000 m (9,800 ft) in 6 minutes 38 seconds
  • Wing loading: 106.7 kg/m2 (21.9 lb/sq ft)
  • Power/mass: 0.2017 kW/kg (0.1227 hp/lb)

Notes

  1. ^ Francillon 1979, p. 204.
  2. ^ a b Francillon 1979, p. 205.
  3. ^ "Warbirds Resource Group". Nakajima Ki-34/L1N1 "Thora". 2010-08-24.

Bibliography

External links

This page was last edited on 18 January 2024, at 16:28
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.