This is a visual explainer based on the Wikipedia article on the Nakajima Type 91 fighter. Read the full source article here. (opens in new tab)

Nakajima Type 91: Forging the Skies of Imperial Japan

An analytical examination of a pivotal early fighter aircraft, exploring its development, specifications, and operational history.

Overview ๐Ÿ‘‡ Specifications ๐Ÿ“

Dive in with Flashcard Learning!


When you are ready...
๐ŸŽฎ Play the Wiki2Web Clarity Challenge Game๐ŸŽฎ

Overview

The Nakajima Type 91

The Nakajima Type 91 fighter was a significant Japanese fighter aircraft developed in the early 1930s. Characterized by its single-engine, single-seat parasol monoplane configuration and a fixed tailskid undercarriage, it represented a key step in the evolution of Japanese military aviation during that era.

Key Specifications

Nakajima Type 91 fighter
General information
TypeFighter
ManufacturerNakajima Aircraft Company
Primary userImperial Japanese Army
Number built450[1]
History
Manufactured1931-1934
Introduction date1931
Retired1937

Design Philosophy

The Type 91 was conceived to meet a specific requirement from the Imperial Japanese Army established in 1927. It evolved from the earlier NC series of prototype fighters. While sharing a lineage, the Type 91 featured a distinct airframe design. Key modifications from its predecessors included a reduced wing size, a repositioned fuel tank, revised wing-bracing struts, the incorporation of a Townend ring cowling for improved engine cooling and aerodynamics, and a redesigned tail assembly and undercarriage system. This iterative design process aimed to enhance performance and handling characteristics for contemporary aerial combat needs.

Development Trajectory

From Requirement to Prototype

The genesis of the Nakajima Type 91 fighter lies in a formal requirement issued by the Imperial Japanese Army in 1927 for a new generation of fighter aircraft. Nakajima Aircraft Company responded by developing the Type 91, building upon the foundational work of their earlier NC series prototypes. The resulting prototype, designated as the sixth machine under the NC designation but representing a significant departure in airframe design, first took to the skies in 1931. This iteration incorporated several critical refinements over the NC series, including a smaller, more efficient wing, a relocated fuel tank for better weight distribution, updated wing-bracing struts, and the adoption of a Townend ring cowling. Furthermore, the tail surfaces and the fixed tailskid undercarriage were redesigned to optimize stability and landing characteristics.

Operational Deployment

Initial Service Challenges

Following its successful first flight, the Imperial Japanese Army officially ordered the aircraft as the Nakajima Army Type 91 fighter. Initial deliveries commenced in late 1931. However, the aircraft's entry into active service was hampered by notable issues concerning directional stability and the aircraft's center of gravity. These aerodynamic challenges necessitated further development and modifications before the Type 91 could be fully integrated into operational units.

Production and Engine Variants

Between 1931 and 1934, a total of 420 Type 91 aircraft were constructed. This production run included approximately 100 units manufactured by Ishikawajima Aircraft Company Limited, highlighting collaborative efforts in Japanese aviation manufacturing. A notable variant, the Type 91-2, was introduced, distinguished by its more powerful Nakajima Kotobuki 2 radial engine, which produced 432 kW (580 hp). This improved version made its maiden flight in July 1934. Despite these advancements, the Type 91 was eventually supplanted in front-line service by the more advanced Kawasaki Army Type 95 fighter during the 1936โ€“1937 period.

Design Variants

Evolution of the Type 91

The Nakajima Type 91 fighter evolved through several distinct variants, each incorporating specific improvements or modifications:

Nakajima NC
This designation refers to the initial prototype and pre-series aircraft. It was powered by the Bristol Jupiter radial engine, delivering 336 kW (450 hp). The NC featured a larger wing compared to the later Type 91 variants and achieved a top speed of 268 km/h. A total of 8 units were built.
Nakajima Army Type 91-1 fighter
This was the primary production version. It utilized a Nakajima-built Bristol Jupiter radial engine, modified to produce between 336 kW and 390 kW (450โ€“520 hp), representing the standard configuration deployed by the Imperial Japanese Army.
Nakajima Army Type 91-2 fighter
An improved variant that incorporated the more powerful Nakajima Kotobuki radial engine. This version offered enhanced performance characteristics and accounted for 21 aircraft in the total production run.

Principal Operators

China

The Republic of China (Nationalist Government) acquired twelve Type 91-1 fighters. These aircraft later saw combat against their former suppliers during the tumultuous Second Sino-Japanese War, underscoring the complex geopolitical landscape of the era.

Japan

The primary operator was the Imperial Japanese Army Air Force, which extensively utilized the Type 91 fighter in its early air power development phase.

Manchukuo

The Manchukuo Imperial Air Force also operated the Type 91 fighter, integrating it into the air arm of the Japanese puppet state.

Enduring Legacy

Preservation Efforts

While the operational service life of the Nakajima Type 91 fighter concluded around 1937, remnants of this historical aircraft are preserved for posterity. A fuselage section is currently on display at the Tokorozawa Aviation Museum in Tokorozawa, Saitama. Additionally, a propeller from a Type 91 is preserved as a historical artifact at the gate of Yanagisawa Shrine in Yamatokลriyama, Nara Prefecture, offering tangible connections to this early chapter of Japanese aviation history.

Technical Specifications

Nakajima Army Type 91-1 Fighter

Data sourced from Japanese aircraft 1910-1941 and The Complete Book of Fighters.

General Characteristics
Length 7.27 m (23 ft 10 in)
Wingspan 11 m (36 ft 1 in)
Height 2.79 m (9 ft 2 in)
Wing area 20 mยฒ (220 sq ft)
Empty weight 1,075 kg (2,370 lb)
Gross weight 1,530 kg (3,373 lb)
Powerplant 1 ร— Nakajima Jupiter VII 9-cylinder air-cooled radial piston engine, 340โ€“390 kW (450โ€“520 hp)
Propellers 2-bladed wooden fixed-pitch propeller
Performance
Maximum speed 300 km/h (190 mph, 160 kn)
Endurance 2 hours
Service ceiling 9,000 m (30,000 ft)
Time to altitude 3,000 m (9,800 ft) in 4 minutes
Wing loading 76.5 kg/mยฒ (15.7 lb/sq ft)
Power/mass 0.21 kW/kg (0.13 hp/lb)
Armament
Guns 2 ร— fixed, 7.7mm Type 89 machine guns

Teacher's Corner

Edit and Print this course in the Wiki2Web Teacher Studio

Edit and Print Materials from this study in the wiki2web studio
Click here to open the "Nakajima Type 91 Fighter" Wiki2Web Studio curriculum kit

Use the free Wiki2web Studio to generate printable flashcards, worksheets, exams, and export your materials as a web page or an interactive game.

True or False?

Test Your Knowledge!

Gamer's Corner

Are you ready for the Wiki2Web Clarity Challenge?

Learn about nakajima_type_91_fighter while playing the wiki2web Clarity Challenge game.
Unlock the mystery image and prove your knowledge by earning trophies. This simple game is addictively fun and is a great way to learn!

Play now

Explore More Topics

Discover other topics to study!

                                        

References

References

A full list of references for this article are available at the Nakajima Type 91 fighter Wikipedia page

Feedback & Support

To report an issue with this page, or to find out ways to support the mission, please click here.

Disclaimer

Important Notice

This page has been meticulously generated by an Artificial Intelligence, drawing upon a comprehensive analysis of publicly available data. It is intended strictly for informational and educational purposes, aiming to provide a scholarly overview of the Nakajima Type 91 fighter. While every effort has been made to ensure accuracy and adherence to the source material, the content represents a snapshot in time and may not encompass all nuances or the most current historical interpretations.

This is not a substitute for professional historical or technical research. The information presented should not be considered definitive or used as the sole basis for academic or professional work without cross-referencing primary sources and expert consultation. The creators of this page assume no liability for any inaccuracies, omissions, or actions taken based on the information provided herein.