The Piasecki X-49 "SpeedHawk" is an American four-bladed, twin-engined experimental high-speed compound helicopter developed by Piasecki Aircraft. The X-49A is based on the airframe of a Sikorsky YSH-60F Seahawk, but utilizes Piasecki's proprietary vectored thrust ducted propeller (VTDP) design and includes the addition of lifting wings. The concept of the experimental program was to apply the VTDP technology to a production military helicopter to determine any benefit gained through increases in performance or useful load.
|X-49A SpeedHawk VTDP Technology Demonstrator in flight|
|Role||Experimental high-speed compound helicopter|
|Manufacturer||Sikorsky (original airframe) |
Piasecki Aircraft (modifications and testing)
|First flight||June 29, 2007|
|Status||Phase 1 complete|
|Primary user||United States Army|
|Number built||1 prototype|
|Developed from||Sikorsky SH-60 Seahawk|
"SpeedHawk" is a concept aircraft based on applying X-49A compounding concepts to a production UH-60 Black Hawk offering better performance, range, and increases in useful load. The "SpeedHawk" aircraft includes an SPU (third engine), high forward-swept wing concept, a 45-inch "fuselage plug" cabin extension, and several other drag reducing and performance-oriented improvements, including a rotor hub fairing, landing gear streamlining, and a fly-by-wire flight control system.
The U.S. Navy-sponsored project, worth US$26.1 million when announced in 2003 ($35.5 million today), consisted of a Sikorsky YSH-60F helicopter modified by Piasecki as a testbed to validate the "Vectored Thrust Ducted Propeller" (VTDP) system. One YSH-60F, powered by two General Electric T700-GE-701C engines, was converted to test the feasibility of VTDP.
The compound helicopter technology installed by Piasecki had been first demonstrated in trials of the Piasecki 16H-1 and 16H-1A “Pathfinder” in the early 1960s, when the helicopters were flown at speeds up to 225 mph (360 km/h). The success of the Pathfinder inspired others to experiment with compounding, resulting in programs such as the AH-56 Cheyenne.
In 2013, it was reported that Piasecki Aviation had made plans to use the VTDP design of the X-49 for their entry in the Future Vertical Lift program, but were not chosen when that project moved into its Joint Multi-Role Technology Demonstrator (JMR-TD) phase.
The X-49A flight demonstrator was developed with funding from the U.S. Army's Aviation Applied Technology Directorate to demonstrate the ability to increase the speed of existing helicopters to 200 kt (360 km/h) or more. The flight demonstrator was updated with a lifting wing taken from an Aerostar FJ-100 business jet. A ring tail was added and the helicopter drive train modified to accommodate VTDP. Piasecki conducted integrated tests of the modified drivetrain at the Navy's helicopter transmission test facility. The wings were intended to produce lift to offload the rotor so the rotor could be slowed down and produce less drag, allowing for higher speed.
The cockpit controls were modified with the addition of a manual propeller pitch override on the collective lever for the ring tail. This is the only visible change to the aircraft's existing mechanical controls in the cockpit. The other controls needed to operate the compound helicopter's systems were integrated into the aircraft's existing mechanical controls to reduce pilot workload. The weight added to the X-49A demonstrator aircraft is estimated at about 1,600 lb (725 kg) due to the requirement to not modify the existing mechanical control system.
The X-49A made its first flight on June 29, 2007 for 15 minutes at Boeing's New Castle County (KILG) flight test center. This flight included hovering, pedal turns, and slow forward and sideways flight using the VTDP for anti-torque, directional and trim control. The X-49A project has been silent since completing its initial testing phase in 2008, with over 80 flight events with and than 80 total hours logged.
Data from 
- Crew: 3
- Length: 64 ft 10 in (19.76 m)
- Height: 17 ft 2 in (5.23 m)
- Empty weight: 13,669 lb (6,200 kg)
- Max takeoff weight: 21,892 lb (9,930 kg)
- Powerplant: 2 × General Electric T700-GE-401C turboshaft engines, 1,620 shp (1,210 kW) each
- Main rotor diameter: 53 ft 8 in (16.36 m)
- Maximum speed: 146 kn (168 mph; 270 km/h)
- Range: 381 nmi (438 mi; 706 km)
- Service ceiling: 19,000 ft (5,790 m)
- Rate of climb: 2,296.5 ft/min (11.666 m/s)
Aircraft of comparable role, configuration and era
- "Piasecki X-49 SpeedHawk (United States)", Jane's Helicopter Markets and Systems. Jane's Information Group, 9 May 2008.
- DOD 4120.15-L - Addendum, Designation-Systems.Net, 8 July 2008.
- Graham Warwick (2006-01-03). "Funding may block X-49 progress". FlightGlobal.com. Retrieved 2007-07-03.
- The Other JMR/FVL Contenders Archived 2013-05-02 at the Wayback Machine - Aviationweek.com, April 12, 2013
- AVX joins Bell, Sikorsky/Boeing for Army's JMR-TD development - Flightglobal.com, 6 June 2013
- Graham Warwick (2007-07-03). "Piasecki flies X-49A SpeedHawk compound helicopter". FlightGlobal.com. Retrieved 2007-07-03.
- Croft, John. Hyper Helos: Prototypes coming off the drawing board and into the race Flight Global, 2008. Accessed: 17 February 2011.
- "Piasecki Achieves First Flight of the X-49A VTDP Compound Helicopter Technology Demonstrator", Piasecki Aircraft, June 29, 2007.
- "Rotorcraft Report: Piasecki SpeedHawk Starts Flight Tests", Rotor & Wing Magazine, August 1, 2007.
- "Piasecki X-49 Speedhawk Technology Demonstrator Compound Helicopter". militaryfactory.com. 18 November 2017. Retrieved 23 November 2017.
|Wikimedia Commons has media related to Piasecki X-49.|
- Official website
- Jane's All The World's Aircraft - X-49A
- "High Speed Helicopter set for first flight in June" article on FlightGlobal.com
- Rotor and Wing Cover Story Dec 2007
- Vertiflite Cover Story Winter 2007
- Aerospace Testing International Dec 2007
- Boeing Eyes X-49A Technology for Apache Attack Helicopter
- "Hot-Rod Helicopters". Air & Space magazine, 1 September 2009.
- Pushing helicopters faster - X-49A - Aviation Week Video