Kaman
H-43
Huskie
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Photo: Robert Deering 1969
Idlewild AAF (A805)
Taegu, Korea
The Kaman HH-43 Huskie was a helicopter with intermeshing rotors used by the United States Air Force, the United States Navy and the United States Marine Corps from the 1950s until the 1970s. It was primarily used for aircraft firefighting and rescue in the close vicinity of air bases, but was later utilized as a short range overland search and rescue aircraft during the Vietnam War. Under the U.S. Navy's pre-1962 aircraft designation system, U.S. Navy and U.S. Marine Corps versions were originally designated as the HTK, HOK or HUK, contingent upon their use as training, observation or utility aircraft.
 
Photo: Robert Deering 10/18/2012
National Museum of the USAF
Wright-Patterson AFB (FFO)

Dayton, Ohio
 

Design and development

In 1947 Anton Flettner, a former German teacher and inventor, was brought to New York in the United States as part of Operation Paperclip.  He was the developer of the former German helicopter Flettner Fl 282 "Kolibri" (Hummingbird), which had the principle of the into each other combing rotors, that solved the problem with the torque compensation. Anton Flettner stayed in the United States and become the chief designer of the Kaman company. He started to design new helicopters, using the Flettner double rotor.

The Huskie had an unusual inter-meshing contra-rotating twin-rotor arrangement with control effected by servo-flaps. The first prototype flew in 1947 and was adopted by the U.S. Navy with a piston-engine. In 1954 in an experiment by Kaman and the US Navy one HTK-1 was modified and flew with its piston engine replaced by two turbine engines becoming the world's first twin turbine helicopter.  Later the Air Force adopted a version with one turboshaft engine: HH-43B and F versions.

Operational history

This aircraft saw use in the Vietnam War with several detachments of the Pacific Air Rescue Center, the 33d, 36th, 37th, and 38th Air Rescue Squadrons, and the 40th Aerospace Rescue and Recovery Squadron, where the aircraft was known by its call sign moniker "Pedro". During Vietnam, the two-pilot HH-43 Huskie flew more rescue missions than all other aircraft combined because of the unique hovering capability. The HH-43 was eventually replaced by newer aircraft in the early 1970s. 

SPECIFICATIONS:  (HH-43F) PERFORMANCE:
Rotor Span:  2× 47 ft in (14.3 m) Maximum speed:  120 mph (190 km/h)
Length:  25 ft 0 in (7.6 m) Cruising speed:  105 mph (169 km/h)
Height:  17 ft 2 in (5.18 m) Range:  185 miles (298 km)
Empty Weight:  Service ceiling:   25,000 ft (7,620 m)
Gross Weight:  9,150 lb (4,150 kg)  
Crew:  Four: two pilots, two rescue crew
Engines:  1 × Lycoming T53 turboshaft, 860 hp (640 kW) each
Armament: 
   
SOURCE: Wikipedia  

Variants

XHTK-1
two two-seat aircraft for evaluation
HTK-1
three-seat production version for the United States Navy, later became TH-43A, 29 built
HTK-1G
one example for evaluation by the United States Coast Guard
HTK-1K
one example for static tests as a drone
XHOK-1
prototype of United States Marine Corps version, two built
HOK-1
United States Marine Corps version powered by a 600 hp R-1340-48 Wasp; later became OH-43D, 81 built
HUK-1
United States Navy version of the HOK-1 with R-1340-52 engine; later became UH-43C, 24 built
H-43A
USAF version of the HOK-1; later became the HH-43A, 18 built
HH-43A
post-1962 designation of the H-43A
H-43B
H-43A powered by a 860shp T-53-L-1B, three-seats and full rescue equipment; later became HH-43B, 200-built
HH-43B
post-1962 designation of the H-43B
UH-43C
post-1962 designation of the HUK-1
OH-43D
post-1962 designation of the HOK-1
TH-43E
post-1962 designation of the HTK-1
HH-43F
HH-43B powered by a 825 shp T-53-L-11A with a reduced diameter rotors, 42 built and conversions from HH-43B
QH-43G
One OH-43D converted to drone configuration