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The Model QH-50APowered by a single 72 HP Porsche engine, the QH-50A was the droned version of Gyrodyne's optimized XRON-1 Rotorcycle which had a 20' rotor diameter.Based on the satisfactory results obtained with the modified automotive Porsche engine, the Navy Bureau of Aeronautics (BuAir) authorized Gyrodyne to enter into negotiations with the Porsche Company of Germany to develop a more suitable engine for the Rotorcycle application. Accordingly, two models were developed, the first one rated at 55 horsepower and the second rated at 72 horsepower. The Porsche engine model rated at 55 horsepower was installed on a rotorcycle with a 17-ft. rotor and was demonstrated at NATC, Patuxent River, Maryland within applicable specifications. The 72-horsepowered model of the Porsche engine was installed on a Rotorcycle incorporating a 20-ft diameter rotor and transmission for the higher horsepower (as seen right). Its first flight was in 1959. This aircraft was also demonstrated at NATC in 1959 and formed the basic airframe for Gyrodyne's entry for the developing unmanned remote-controlled helicopter requirement the Navy was seeking to fulfill. This helicopter also won the Grand Prize for the most maneuverable helicopter in the 1961 Paris Air Show at Le Bourget, France. Despite Gyrodyne's success in the development of its one-manned, compact helicopter for the Marine Corps, the Navy believed that the stability and reduction of size afforded by the coaxial rotor system made the helicopter's design best utilized as a drone. In June of 1958, the Chief of Naval operations determined that operational drone helicopters would be required in the fleet beginning in fiscal year 1962. To meet this requirement, it was planned that the DASH program should proceed on a three-phase basis. The first phase would be to buy an initial quantity of nine DSN-1 (later QH-50A designation) (as seen left) and three DSN-2 (later QH-50B designation) helicopters for research and development purposes. The second phase would be to buy a larger limited number of twin engine DSN-2 (later QH-50B designation) helicopters. It was planned that these drones would be used in the fleet beginning in July 1961 until the more advanced drone, the DSN-3 (later QH-50C designation) could be delivered to the fleet. The third phase of the program would be a design competition which would lead to the production of operational quantities of the QH-50C drone. Under this plan, fleet deliveries of the QH-50C were to begin after July 1963. Accordingly, in
keeping with it's plan, the Navy issued its authorization to proceed with
the droning of the XRON-1 helicopter as the model QH-50A drone (seen
right) on December 31,
1958, under Contract NOas 59-0219-c in order to initiate the DASH program. The
award was a cost-plus-a-fixed-fee contract which covered the initial purchase of
the nine DSN-1 and three DSN-2 aircraft. Under this contract deliveries to the
Navy occurred from June 1960 through December 1961.
The QH-50A goes into ProductionThe
QH-50A was to be the evaluation prototype for the airborne portion of the system
and be capable of carrying one Mark 43 homing
torpedo. During the development of the remotely controlled helicopter, Gyrodyne had used the assistance of a safety pilot in order to abbreviate the development time of the autopilot and remote control equipment and also provide for safety of flight during the developmental stages. As seen at right, a QH-50A makes its approach to the destroyer, USS Hazelwood (DD-531) off the coast of Key West, Florida on September 12, 1960.
The QH-50B goes into Production but gets Cancelled.In the summer of 1959, the Navy's Ships Characteristics Board decided that aviation gasoline, a fire hazard aboard destroyers, should be removed from destroyers that were able to carry DASH drones. Since the DSN-2 drones (seen left with safety pilot) used gasoline powered Porsche engines, the Chief of Naval Operations directed that the planned DSN-2 (later QH-50B designation) production procurement for fiscal year 1960 not be made and that the QH-50C turbine-powered drone, using the less dangerous jet fuel, be placed into development. Subsequently, only the original three DSN-2 aircraft were ever produced and remain at Gyrodyne to this date, as non flyable airframes. After all DASH work was shifted from the gasoline burning QH-50A/B models and to the jet fuel burning QH-50C, the A models were eventually used as targets at Point Magu, California in 1965 for missile testing. Only 2 survive to this date and they are in private collectors hands. As the QH-50A remains today and did in 1960 as a valid and viable choice as an entry level coaxial platform, we supply the following data for those interested in the light-weight and compact A model.
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Serial Number HistoryQH-50B Drone (referred to DSN-2 prior to 1962)The Three Aircraft were ordered under Contract NOas 59-0219-c, Amendment 1 |
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Serial Number |
Number Produced |
Acceptance Date |
DASH Program Use |
Disposition |
N-200 | 1 |
October 1960 |
Ground Tests conducted by Gyrodyne |
N-200 was used for a 25 hr. ground test. It served for 5 months until retirement in February 1961. |
N-201 | 1 |
November 1960 |
Flight Envelope and N-202 back-up; used by Gyrodyne |
Serving for 11 months, this manned-drone continued to expand the flight envelope to qualify the DSN-2 to DASH specifications. It was retired in October 1961 |
N-202 | 1 |
December 1960 |
Checkout of First DSN-3 Digital control group by Gyrodyne |
Picking up where N-201 left off, N-202 was the test bed for the QH-50C's automatic flight control system including shipboard checkout of LAD up to sea state 3 |
All three DSN-2 aircraft were scrapped in 2002 |
PERFORMANCE SUMMARY |
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QH-50B Drone |
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Take-Off Loading Conditions-ASW Attack, Full Fuel | |||||||||||
QH-50B First flight on September 30, 1960 | |||||||||||
Power Plant |
Weights | ||||||||||
Engine | Empty | 819 lbs | |||||||||
Manufacturer | Porsche, Model YO95-6 | Maximum Gross | 1450 lbs | ||||||||
Type | 4 cylinder, 4 cycle, Reciprocating | Fuel (11 gallons) | 66 lbs | ||||||||
Quantity | Two | Oil | 22 lbs | ||||||||
Horsepower | Total 144 hp | Payload | 543 lbs | ||||||||
Performance |
Fuel Consumption | Fuel and Oil | |||||||||
Speed |
Knots | Speed | Lbs/hr. | Fuel Tanks | One | Gallons | 11.0 gal. | ||||
Vmax at S.L. | 76.8 | at Vmax |
81.2 |
Grade | 100-LL | Location | Fwd- Trans | ||||
V cruise | 63.0 | at cruise |
63.0 |
Oil Spec | 30 weight | Oil Capacity | 8 quarts | ||||
Rate of Climb |
Hovering Ceiling |
Endurance & Range |
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Vertical | 640 ft/min. | Out of Ground Effect | 2,950 ft. | Maximum Endurance | 1.06 hr. | ||||||
Maximum with Forward Speed | 1,162 ft./min. | Service Ceiling | 8,600 ft. | Maximum Range | 68 n. miles | ||||||
Dimensions |
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Lengths |
Widths |
Height & Rotor |
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Max Length (rotors) | 20 ft. 0 inches | Width (skids) | 5 ft. 7 inches | Height (overall) | 8 ft. 3 inches | ||||||
Length (fuselage) | 7 ft. 0 inches | Width (fuselage) | 4 ft. 6 inches | Rotor Diameter | 20 ft. 0 inches | ||||||
Ordnance |
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Weapons: | MK-43 single Torpedo | ||||||||||
or, external payload | 500 lbs |
The name "Gyrodyne" in its stylized
form above, is the Trademark of and owned by the Gyrodyne Helicopter Historical
Foundation; unauthorized use is PROHIBITED by Federal Law. All Photographs, technical specifications, and
content are herein copyrighted and owned exclusively by Gyrodyne Helicopter
Historical Foundation, unless otherwise stated. All Rights Reserved
©2013. |