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Hiller OH-23 Raven (Model UH-12)


Light Utility Helicopter (LUH) (1948)


Aviation / Aerospace

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Jump-to: Specifications

Despite its rather simple appearance, the Hiller OH-23 Raven light helicopter line proved reliable even under the wartime stresses of Korea and Vietnam.



Authored By: Staff Writer | Last Edited: 05/20/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.
Hiller Aircraft began during World War 2 in 1942 under the operating name of Hiller Industries. The company carried the surname of Stanley Hiller (1924-2006) whose provided much of the early work in the field of helicopter flight. Indeed his first coaxial helicopter design was completed at age 15 and his XH-44 impressed the US Army at age 17. Hiller headed the first helicopter factory in the world out of Berkeley, California. Among his early developments (now under the "United Helicopters" name) included the UH-4 "Commuter" and the UH-5B "Rotormatic" which led to the single-seat UH-12 light utility helicopter of the late 1940s.

The UH-12 held origins in the company Model 360 and saw a first flight in 1948. The UH-12A was a follow-up modification to the original UH-12 and included a more powerful engine to go along with a new, two-blade main rotor. The US Army liked what it saw and contracted for a militarized variant of the UH-12A and this became the evaluation prototype designated YH-23. For the military form, crew capacity was increased to two in a side-by-side seating arrangement underneath a largely transparent bubble-style windscreen. The aircraft was powered by a single Franklin piston engine of 178 horsepower.

The overall configuration consisted of a front-mounted cockpit (originally single-seat and then seating for two or more) with a mid-mounted engine and rear-set stem. The engine powered a two-bladed main rotor blade fitted high atop the mast and drove a two-bladed tail rotor used to offset torque. The cockpit offered generally excellent vision and the undercarriage was of a basic skid-type design. While typically unarmed, some war-time models were outfitted with 2 x 0.30 caliber medium machine guns for basic offense.

Following successful trials of the YH-23, the system was formally adopted by the US Army as the H-23A "Raven" across 100 examples. The powerplant became the Franklin O-335-4 piston engine outputting at 178 horsepower. The type also piqued the interest of the USAF whom ordered five examples for official evaluation. The H-23A was followed into service by the revised H-23B. This new model series incorporated a combined skid-and-wheel undercarriage and was powered by a Franklin O-335-6 series piston engine of 200 horsepower output. The US Army then took on a stock of 273 units while an additional 81 served the export market. Some later OH-23B models were upgraded to the more powerful Lycoming VO-435-23B series engine of 250 horsepower.

The H-23C proved unique upon its arrival for it featured seating for three personnel under a single-piece canopy cover and also instituted use of metal blades. Some 145 were procured by the US Army. The H-23D was given an all-new main rotor design and powerpack to include the Lycoming VO-435-23B engine of 250 horsepower. US Army procurement numbered 348 examples. The H-23E was offered but never purchased.

The H-23D seated two crew and showcased a maximum speed of 95 miles per hour with a cruise speed reaching 82 miles per hour. It fielded a range of 200 miles with a service ceiling of 13,200 feet. A rate-of-climb of 1,050 feet was reported.
The H-23F became a four-seat model with enlarged crew cabin. Additional changes included the use of the VO-540-A1B engine of 305 horsepower. The following H-23G offered seating for three personnel and dual-control features for both pilot positions. This mark was largely based on the preceding H-23F line.

The US Navy followed its own naming convention and tagged the UH-12A as the HTE-1. They were also two-seat airframes but offered dual-controls for both positions. Interestingly, this mark also showcased a tricycle-style wheeled undercarriage. Seventeen of the type were manufactured. The HTE-1 was then followed by the HTE-2 which was the H-23B and its Franklin O-335-6 piston engine of 200 horsepower. 35 examples were procured.

The Royal Navy followed suit and purchased the Hiller design under two marks - Hiller HT.Mk 1 and HT.Mk 2. The Mk 1 were ex-US Navy mounts (HTE-2 models) while the Mk 2 were UH-12E production models. Numbers totaled 20 and 21 respectively and primarily held as trainers out of RNAS Culdrose (Cornwall). The Canadian Army utilized the Hiller design as well, this under the C-112 "Noman" designation.

In 1962, the United States military underwent a branches-wide designation revision which changed all H-23 designations to the "OH" format. H-23B became OH-23B, H-23C became OH-23C and so on (see variants section for complete list). Many OH-23 variants were based on existing civilian-minded Hiller marks including the original UH-12A. The UH-12B was the basis for the US Navy HTE-1 while the UH-12C was the H-23C. The UH-12 was the H-23D and so forth.

The OH-23 proved exceedingly popular on the world market beyond its use by the United States, United Kingdom and Canada. The list included Argentina, Chile, Indonesia, Israel, Mexico, the Netherlands, South Korea, Thailand and Uruguay among others.

The OH-23 served American forces during the Korean War (1950-1953) as one of the handful of helicopters present in the conflict. The conflict marked the first practical use of rotary-wing aircraft in a modern war despite their (limited) use in the latter years of World War 2. The Hiller aircraft was used in the mission liaison, scouting, observation, general service, trainer and MEDEVAC role in the war, operated alongside the similar Bell Model 47/H-13 "Sioux" helicopter lines. The primary military variant became the OH-23D. As with the H-13 line, the OH-23 saw some combat service in the early years of the Vietnam War. They were replaced, in time, by the much improved Hughes OH-6A "Cayuse" light helicopter.

Specifications



Service Year
1948

Origin
United States national flag graphic
United States

Status
RETIRED
Not in Service.
Crew
1

Production
1,820
UNITS


Hiller Aircraft Corporation - USA
National flag of Argentina National flag of Canada National flag of Chile National flag of Colombia National flag of the Dominican Republic National flag of Indonesia National flag of Israel National flag of Mexico National flag of the Netherlands National flag of Peru National flag of South Korea National flag of Thailand National flag of the United Kingdom National flag of the United States National flag of Uruguay Argentina; Canada; Chile; Colombia; Dominican Republic; Guatemala; Indonesia; Israel; Mexico; Netherlands; Paraguay; Peru; South Korea; Thailand; United Kingdom; United States; Uruguay
(OPERATORS list includes past, present, and future operators when applicable)
Close-Air Support (CAS)
Developed to operate in close proximity to active ground elements by way of a broad array of air-to-ground ordnance and munitions options.
Special-Mission: MEDical EVACuation (MEDEVAC)
Extraction of wounded combat or civilian elements by way of specialized onboard equipment and available internal volume or external carrying capability.
Special-Mission: Search & Rescue (SAR)
Ability to locate and extract personnel from areas of potential harm or peril (i.e. downed airmen in the sea).
Intelligence-Surveillance-Reconnaissance (ISR), Scout
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.
Training (General)
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).


Length
27.8 ft
(8.47 m)
Width/Span
35.4 ft
(10.80 m)
Height
9.8 ft
(3.00 m)
Empty Wgt
1,819 lb
(825 kg)
MTOW
2,712 lb
(1,230 kg)
Wgt Diff
+893 lb
(+405 kg)
(Showcased structural values pertain to the Hiller H-23D Raven production variant)
Installed: 1 x Lycoming VO-435-23B 6-cylinder engine developing 250 horsepower driving a two-bladed main rotor unit and two-bladed tail rotor unit.
Max Speed
95 mph
(153 kph | 83 kts)
Ceiling
13,205 ft
(4,025 m | 3 mi)
Range
197 mi
(317 km | 587 nm)
Rate-of-Climb
1,050 ft/min
(320 m/min)


♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


(Showcased performance specifications pertain to the Hiller H-23D Raven production variant. Compare this aircraft entry against any other in our database. View aircraft by powerplant type)
Usually none though some wartime models were outfitted with 2 x 0.30 caliber (7.62mm) Medium Machine Guns (MMGs) in special outboard mountings.


Supported Types


Graphical image of an aircraft medium machine gun


(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 0


H-23 "Raven" - Base Hiller company model designation
YH-23 - U.S. Army evaluation model; single example
H-23A - Initial production model; powered by Franklin O-335-4 engine; two-seat; 105 produced.
H-23B - Powered by Franklin O-335-6 engine of 200 horsepower; 354 produced.
H-23C - Three-seater; metal main rotor blade; 145 examples.
H-23D - All-new main rotor; powered by Lycoming VO-435-23B engine of 250 horsepower; new transmission; 348 produced.
H-23E - Proposed variant; not adopted
H-23F - Four-seater; Lycoming VO-540-A1B engine of 305 horsepower; 22 produced.
H-23G - Three-seater with dual control scheme; 793 examples produced.
HTE-1 - USN model; Franklin O-335 engine; dual control scheme in two-seat cockpit arrangement; wheeled undercarriage; 17 examples produced.
HTE-2 - USN model; Franklin O-335-6 engine; 35 examples produced.
HT Mk 1 - British Navy designation; 20 examples from USN stock.
HT Mk 2 - British Navy designation; 22 examples
CH-112 "Nomad" - Canadian Army designation
U-12A (H-23A) - Civilian model; Franklin O-335-4 engine of 178 horsepower.
UH-12B - USN trainer
UH-12C - Three-seat variant
UH-12D - Improved H-23C for US Army service
UH-12E - Three-seater with dual control scheme
UH-12ET - UH-12E with Allison 250 series turboshaft engine.
UH-12E3 - Improved three-seat form
UH-12E3T - Improved turboshaft version
UH-12E4 - Four-seater; Lycoming VO-540 engine
UH-12E4T - Four-seater with turboshaft engine
UH-12L-4 - Extended fuselage; enlarged cabin windows


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