Hiller 1033 / XROE-1 Rotorcycle

On January 10, 1957, the US Navy announced the successful first flight of the one man collapsible Rotorcycle, developed for the US Marine Corps by Hiller Helicopters of Palo Alto, California. Hiller was one of two companies selected during 1954 to design and build a one man helicopter but the idea was not wholly successful and it failed to achieve full production status after initial flight testing was completed by July 1957.
Designated XROE 1, this was a unique one-man helicopter which could fold into a small package for easy transportation or parachute delivery. Weighing less than 250 lbs it was powered by a Nelson four cylinder opposed, two cycle, air cooled petrol engine manufactured by Barmotive Products Inc a single rotor, eighteen feet in diameter and positioned above the pilot’s head, provided lift, with a small tail rotor located in a tubular boom compensating for torque. The entire helicopter was held together by quick release pins and could be assembled by one person.
Although not literally a ‘strap on the back’ machine, the XROE 1 approximated closely to this idea, since the pilot sat on what appeared to be a bicycle seat, with the engine just behind him. The US Marine Corps intended to use the XROE 1 for observation, liaison, small tactical missions, such as escape and evasion, pilot rescue and any other James Bond’ type drama.

Transmission of the Rotorcycle incorporated a single spiral bevel gear set and an over-running clutch while the fuel system was of the gravity feed type. Official Marine Corps specification data indicated that the XROE 1 could be folded or assembled in the field in less than five minutes and, for aerial drops to downed pilots or stranded troops, the folded Rotorcycle fitted into a streamlined container suitable for external transportation on a fixed-wing aircraft. It was expected to enter service by Septembr 1959.

During May 1958, while on a European sales tour, the Hiller XROE 1 Rotorcycle was demonstrated at Elstree aerodrome, Herts. On this occasion, two men assembled the machine in just three minutes, a rather slow time according to the manufacturers who stated that the record stood at one minute fifty seconds. Although based around a Marine Corps specification, the XROE 1 was evaluated by both Germany and Switzerland, the licensee in Europe being Helicop Air of Paris and the estimated cost was $10,000 for production machines.

Demonstration in England 1955

In November 1958, a contract was signed for a batch of ten Rotorcycles to be built by Saunders Roe at its Eastleigh, Southampton factory, on the basis that it would cost less to build a small batch of XROE 1s in the United Kingdom than in the USA. Helicop Air of Paris, Hiller’s agent in Europe, was responsible for handling the contract which was quite unique.

Using materials from the USA, Saunders Roe built the jigs and tools, manufactured the gearing, transmission components and the structure. All proprietary items, including the engine, electrics, main rotor blades and instruments, were also supplied from the USA. The Rotorcycles were completed in accordance with Hiller drawings.

Saro-built Rotorcycle

The control technique was known as the Hiller Rotormatic system while, in place of a landing gear, the Rotorcycle was supported on three tapered aluminium alloy spring tubes.

The fate of the majority of the XROE 1 Rotorcycles after leaving the Eastleigh factory of Saunders Roe is not known, but the type was evaluated for the Marine Corps at the Naval Air Test Centre and the published performance figures are based on this evaluation. Three Rotorcycles all designated YROE 1 were also assessed by NASA at their Ames facility at Moffett Field, California, YROE 1s ‘4020’ ‘4021’ and ‘4024’ being delivered there on November 16, 1962. The serial numbers applied to the YROE 1s tonsisted of four digits only, this system not conforming to the more familiar BuNo’s as used by the Bureau of Aeronautics to identify US Navy and US Marine Corps aircraft and helicopters.
Two examples of the Hiller YROE 1 Rotorcycle reside in museums situated within just a few miles of each other. The first specimen ‘4020’ is in a private museum owned by James S Ricklefs of Rick Helicopters Inc. of San Carlos, California. This one has an intact manufacturer’s plate which revealed the following interesting information: Manufacturer’s model 1033: Customers model YROE4: Serial No 6: Customer’s serial No 4020: Contract No 59 6022: Engine type YO 65 2. Accepted 21 June 1960. Manufactured by Saunders Roe Lid. England under agreement from International Engineering Research & Development, Luxembourg under licence from Hiller Aircraft Corporation, USA. Restored by John Trome 1980.
The second YROE 1, 14021′, was discovered in The Flying Lady Museum which is owned by Irv and Jan Perch and located at Morgan Hill, near South County Airport, some 65 miles south of San Francisco.

Hiller

Hiller Industries
Hiller Helicopters
Hiller Aviation
Rogerson Hiller Corporation
Hiller Aircraft Corporation

Hiller Helicopters Inc. was formed in 1942 for the development and production of rotary-wing aircraft. Early work on the Hiller Model XH-44, UH-4 Commuter and the UH-5, which introduced a newly-developed ‘Rotor-Matic’ rotor control system, led to the Hiller Model 360 prototype.
Stanley Hiller flew the first successful American co-axial helicopter, the XH-44, in July 1944, when he was only 19 years old. It also featured the world’s first successful all-metal rigid-rotor blades. Hiller had learned to fly from his father at an early age, and at 16, Hiller had started a business building small gasoline engine model cars; revenue eventually grew to $100,000. Hiller became interested in helicopters in 1937 when he saw pictures of the Focke Wulf Fw 61 and Sikorsky’s VS-300 in 1939. Hiller felt the tail rotors used on the VS-300 and the outriggers on the Fw 61 were wasteful and possibly unnecessary.
Formed 1942 as a division of Hiller Industries. Name changed to Hiller Helicopters in 1948.

In 1948 Hiller Helicopters produced the Hiller UH-12, subsequently supplying it to civilian operators and, as the H- 23B and OH-23C/D Raven, to the U.S. Army and to foreign air arms under the MDAP program . Three-seat UH-12E (first flown 1958) and four-seat UH-12E4 variants also developed. The Hiller HOE-1 Hornet ramjet ultralight helicopter and “Flying Platform” were two military experimental types devised by the company.

In 1964 Fairchild-Stratos Corp purchased Hiller Aircraft with cash, not stock transactions. Hiller capabilities fitted into one of Fairchild’s primary goals – vertical takeoff and landing aircraft. The Hiller plant was to remain in Palo Alto.

Fairchild Stratos Corporation acquired Hiller in 1964, hence the FH designations, believing they were about to secure a large military contract as the OH-5A stood out the preferred winner. Leaked production data of the OH-5A resulted in Howard Hughes successfully under bidding with the OH-6A. Fairchild meanwhile announced they would begin civilian helicopter production of a refined OH-5A, designated the FH1100.
Hiller Aviation Inc was formed in 1973 after acquiring the design rights, tooling and spares for Hiller 12E light helicopters from Fairchild Industries. The company provided support for operators of Hiller helicopters and produced three-seat UH- 12E and four-seat UH-12E-4 turbine conversions of the UH-12E, developed in conjunction with Soloy Conversions. Also introduced former Fairchild Hiller FH-1100 in 1984 (later as RH-1100). Became subsidiary of Rogerson Aircraft in 1984, reviving first the name Hiller Helicopters and later becoming Rogerson Hiller Corporation.

Hiller Aircraft Corporation was founded 1994 by Jeffrey Hiller (son of the founder of the original Hiller Aircraft company) and a consortium, to repurchase assets from Rogerson Hiller Corporation. First flight January 1995 of the UH-12E5 five-seat helicopter, and June 1995 for first newly built UH-12E3.

1995: 2140 West 18th St, Port Angeles, Washington 98362, USA.

Hillberg Turbine Exec

The Turbine Exec is a turbine kit to repower the Rotorway Executive kit helicopter. First flown in April 1997, the US$20,000 kit included the engine, gearbox reduction drive and tail rotor gearbox.

Max speed: 125 mph
Cruise: 100 mph
Range: 225 sm
Rate of climb: 1500 fpm
Service ceiling: 13,500 ft
Engine: Solar T6Z-T32
hp range: 150-170
Fuel capacity: 35 USG
Empty weight: 750 lb
Gross weight: 1425 lb
Height: 8 ft
Length: 22 ft
Disk span: 25 ft
Seats: 2

Hillberg EH1-02

The first flight was scheduled for the Spring of 1998.
Kits were to include everthing except radios, with plans selling for US$350, and kit for US$68,000.

Max speed: 170 mph
Cruise: 130 mph
Range: 390 sm
Rate of climb: 1500 fpm
Service ceiling: 13,500 ft
Engine: Solar T6Z-T32
hp range: 150-400
Fuel capacity: 45 USG
Empty weight: 900 lb
Gross weight: 1800 lb
Height: 8 ft
Length: 28 ft
Disk span: 25 ft
Seats: 2

Hillberg RotorMouse EH1-01

A turboshaft powered helicopter first flown in 1994. The first kit was shipped in January 1998. Plans were selling at US$350 and the kit price was US$68,000. Of aluminium construction, the Solar T62T32 or other engines with 150-225 hp are suitable.

Max speed: 160 mph
Cruise: 130 mph
Range: 300+ sm
Rate of climb: 4700 fpm
Engine: AiResearch, 145 hp
hp range: 145-250
Fuel capacity: 32.9 USG
Empty weight: 635 lb
Gross weight: 1300 lb
Height: 7.4 ft
Length: 20.1 ft
Disk span: 20 ft
Disk area: 314.2 sq.ft
Seats: 1

Hillberg Helicopter

1997: PO Box 8974, Fountain Valley, CA 92728-8974, USA.

In addition to helicopter maintenance and modification, offered the RotorMouse EH 1 -01 as a single-seat turbine experimental-category helicopter for construction from a kit (first flown August 1993), RotorMouse EH 1 -02 tandem two-seat version, and RotorMouse (Baby Huey) four-seater. Also built the T-4 Turbine as a four-seat turbine helicopter, and produced a retrofit kit for the RotorWay Exec to provide a turbine engine (first flown 1997).

Hill Voyager

Klaus Hill designed the Manta Fledglings. When Manta made the Fledgling-II, Klaus was not happy with the results, so he did it better: this was the Voyager.

Klaus combined the Kasper wingtip gates and Fledgling rudders to make effective NASA winglets for the Fledgling hang glider.

Klaus Hill was killed on 10 October 1978 while testing the Voyager, a hang glider of his own design, which he had just motorised.

Hill Pterodactyl

A series of tailless aircraft was designed by Professor Geoffrey Hill to demonstrate the concept of aircraft that could fly safely at low speed. The first machine was a glider which he built in 1924 and flew from the South Downs, UK. From this a powered version was constructed.

Hild-Marshonet 1918 biplane

The Hild-Marshonet biplane was designed and built by Frederick Hild and Edward Marshonet of Hempstead, New York, in 1919. It had no fuselage as such, the pilot being seated in a streamlined nacelle. An outrigger of boxed cantilever construction supporting the empennage was attached directly behind the pilot’s seat. It had a single-boom tail and swept back wings.

It was powered by a 20 hp-Spainhour V-twin engine.

The plane could be taken apart in minutes.

Span: 24 ft
Length: 19 ft
Empty weight: 450 lb
Loaded weight: 700 lb
Speed: 65 mph
Price $2,000.