Bell 48 (H-12)

In 1946, the “Bell” company began developing a new military helicopter, which was essentially an enlarged version of the Model 47. The Model 48 machine was created based on the unsuccessful Model 42, intended for the civilian market.

Development and Early Prototypes

The U.S. Army Aviation ordered two prototypes of the five-seat XR-12, powered by a 540 hp (403 kW) Pratt & Whitney R-1340-AN-1 radial engine. There was also a slightly larger 12-seat prototype, the XR-12B (Model 48A), with a more powerful Wasp powerplant variant.

Due to a change in helicopter designations, the XR-12 and XR-12B became the XH-12 and XH-12B, respectively.

Challenges and Production Cancellation

Serious problems arose during the development process of the XR-12, leading to the cancellation of the order for 34 R-12A production aircraft. The first XR-12B was followed by 10 YR-12B (later YH-12B) with a more powerful R-1340-55 radial engine. Continued development difficulties resulted in no orders being placed for the production H-12B.

Technical Specifications

Modification	YH-12B
Main rotor diameter, m	14.48
Tail rotor diameter, m	2.59
Length, m	12.06
Height, m	3.43
Maximum takeoff weight, kg	2854
Engine type	1 Piston engine Pratt & Whitney R-1340-55
Power, kW	1 x 447
Maximum speed, km/h	168
Cruising speed, km/h	145
Practical range, km	480
Rate of climb, m/min	137
Service ceiling, m	3960
Static ceiling, m	1330
Crew, crew	1-2
Payload	up to 10 passengers

Image and diagram gallery of the Bell 48 (H-12)

Bell 48 (H-12)	Bell 48 (H-12)
Bell 48 (H-12)	Bell 48 (H-12)
Bell 48 (H-12)	Bell 48 (H-12)