McCulloch J-2
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{{Infobox aircraft
|name=J-2
|image=McCulloch_J-2_Aero_Super_Gyroplane_-_GPN-2000-001904.jpg
|caption=
|type=Civil utility autogyro
|manufacturer=McCulloch, Aero Resources
|designer=Drago Jovanovich
|first_flight=June 1962
|introduction=
|retired=
|status=
|primary_user=private pilot owners
|more_users=
|produced=
|number_built= at least 83
|variants=
}}
The McCulloch J-2 was a small, two-seat autogyro with an enclosed cabin, one of only three designs of this type of aircraft to receive a type certificate in the United States. It was built by McCulloch Aircraft Corporation.
Design and development
It was designed by Drago Jovanovich and first flew in June 1962. McCulloch acquired the design in 1969 and put it into production, building 83 aircraft over the next three years. They were reported to sell for US$15,900.For you and your gal - an autogyro, Ken W Purdy, Albuquerque Journal, 8 June 1969, page 108
The design featured a belt clutch and a transmission which could be engaged to spin the rotor blades to high speed before take-off to produce short takeoff runs. A lever on the rear cockpit wall would select the drive position for the transmission. A single "spin-up lever" on the cockpit left side would then be pressed downward, operating as a collective pitch control to put the blades into flat pitch while simultaneously tensioning the belt clutch. The rotor could be spun to over 500 rpm before takeoff, well above the normal flight range (typically 425 rpm). Release of the spin-up lever would disengage both the clutch and the transmission, while placing the blades into flight pitch. After a very brief takeoff run (typically 25 to 200 feet, depending upon load and winds) adequate flight airspeed would be attained, while the rotor speed decayed to the normal flight range. The rotor was not engine-driven in flight. A strong spring resisted accidental depressing of the spin-up lever while airborne. Dual controls were provided for all functions except the spin-up lever, which was accessible only from the left seat. The aircraft enjoyed nimble handling with light control forces, but suffered from a shallow climb gradient.{{Citation needed|date=January 2017}}
File:McCulloch J-2 G-AZWZ SYW 08.07.73 edited-2.jpg
Early versions were equipped with a two-bladed wooden Sensenich propeller. A later "Super J-2" variant employed a three-bladed Hartzell controllable-pitch propeller, accompanied by an increase in allowable gross weight. Baggage of up to 95 pounds, to the extent permitted by gross weight considerations, could be carried in a large bay under the seat. Fuel was carried in tanks in the stub wings. A total of 24 U.S. gallons could be carried, 12 on each side, but only 20 were usable through normal flight attitudes. At a typical fuel burn rate of about eight gallons per hour and economy cruise at about 85 mph, with a need for a safety reserve, this limited the aircraft's range.{{Citation needed|date=January 2017}}
The rotor system (hub and blades) is very similar to that found on the early versions of the Hughes 269 / Schweizer 300 series helicopters. The primary difference is in the twist of the blades (or lack thereof), optimized for autorotation in the case of the J-2.{{Citation needed|date=January 2017}}
Most examples of the J-2 were sold to pilot owners in the United States but at least one example was exported to the United Kingdom.[https://cwsprduksumbraco.blob.core.windows.net/g-info/HistoricalLedger/G-AZWZ.pdf UK Register of Civil Aircraft - register entry for G-AZWZ (pictured)]
In 1974, the rights were bought by Aero Resources, who planned to return the Super J-2 to production, but could not find a market for the aircraft and no more were built.{{Citation needed|date=January 2017}}
Variants
;Jovanovich Jov-2
:The initial prototype as designed by Drago Jovanovich.{{Citation needed|date=January 2017}}
;McCulloch J-2 and Super J-2
:Production versions built by McCulloch from 1971 to 1974. 83 built.{{Citation needed|date=January 2017}}
;Aero Resources Super J-2
:Further planned production by Aero resources, powered by a {{convert|180|hp|kW|abbr=on|0}} Lycoming O-360-A2D. None built.{{Citation needed|date=January 2017}}
Aircraft on display
Specifications (Super J-2)
{{Aircraft specs
|ref={{Citation needed|date=January 2017}}
|prime units?=imp
|genhide=
|crew=one pilot
|capacity=one passenger
|length m=4.8
|length ft=
|length in=
|length note=
|span m=
|span ft=
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|height m=
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|wing area sqm=
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|wing area note=
|airfoil=
|empty weight kg=503
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=725
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|eng1 number=1
|eng1 name=Lycoming O-360-A2D
|eng1 type=4-cyl. horizontally opposed
|eng1 kw=
|eng1 hp=180
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
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|prop note=
|rot number=1
|rot dia m=7.9
|rot dia ft=
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|rot area sqm=49
|rot area sqft=
|rot area note=
|perfhide=
|max speed kmh=171
|max speed mph=
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|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=320
|range miles=
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|endurance=
|ceiling m=2,440
|ceiling ft=
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|roll rate=
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|climb rate ms=3.5
|climb rate ftmin=
|climb rate note=
|time to altitude=
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|wing loading kg/m2=
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}}
See also
References
{{Reflist}}
- {{cite book |title=Approved Rotorcraft Flight Manual, Report No. J-2-100|year=1972 |publisher=Aero Resources, Inc.|location=Gardena, CA|pages=39}}
- {{cite book |title=Type Certificate Data Sheet H6WE, Rev. 1|year=1973 |publisher=Federal Aviation Administration |location=Washington, DC}}
- {{cite book |title=The J-2 Gyroplane and how to fly it|year=1970 |publisher=McCulloch Aircraft Corporation |location=Lake Havasu City, AZ |pages=44}}
{{commons category|McCulloch J-2}}
- {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=31}}
- {{cite book |last= Gunston |first= Bill |title=World Encyclopedia of Aircraft Manufacturers |year=1993 |publisher=Naval Institute Press |location= Annapolis |pages=162}}
- [https://web.archive.org/web/20050601045421/http://www.aerofiles.com/_ab.html Aerofiles]
- {{Internet Archive short film|id=gov.ntis.ava08353vnb1|name=Airports Mean Business (1972)}}
{{McCulloch aircraft}}
http://www.gyroplane.co/gyro_article_2003.html
Category:1960s United States civil utility aircraft
Category:Single-engined pusher autogyros