Boeing–Sikorsky RAH-66 Comanche(Redirected from RAH-66 Comanche)
The Boeing–Sikorsky RAH-66 Comanche is an advanced five-blade armed reconnaissance and attack helicopter designed for the United States Army. Following decades of development, during 2004, the RAH-66 program was canceled prior to mass production commencing, by which point nearly US$7 billion had been already spent on the program.
|The first RAH-66 prototype during its maiden flight on 4 January 1996|
|Role||Reconnaissance and attack helicopter|
|National origin||United States|
|Manufacturer||Boeing Helicopters/Sikorsky Aircraft|
|First flight||4 January 1996|
|Primary user||United States Army|
|Program cost||US$6.9 billion (2004)|
During the early 1980s, the U.S. Army started to formulate requirements for the replacement of its helicopters then in service, which resulted in the launch of the Light Helicopter Experimental (LHX) program. Nearly a decade later, following the refinement of requirements, evaluation of submissions, and the rebranding of the programme as the Light Helicopter (LX) program, during April 1991, the Army announced the selection of the Boeing–Sikorsky team's design as the contest winner, shortly after which a contract for construction of prototypes was awarded. The Comanche was to incorporate several advanced elements, such as stealth technologies, and a number of previously untried design features. Operationally, it was to employ advanced sensors in its reconnaissance role, where it was intended to designate targets for the AH-64 Apache. It was also armed with one rotary cannon and several missiles and rockets for light attack duties.
A pair of RAH-66 prototypes were constructed and underwent flight testing between 1996 and 2004. On 1 June 2000, it was announced that the program had entered its $3.1 billion engineering and manufacturing development (EMD) phase. However, during 2002, the Comanche program underwent heavy restructuring; the number of Comanches that were to be purchased was cut to 650. At the time, the projected total cost for the full production of the Comanche in such numbers stood at $26.9 billion. As early as the late 1990s, the Government Accountability Office (GAO) had reported that it had "serious doubts" about the program, observing that the Comanche would "consume almost two thirds of the whole Aviation budget by Fiscal Year 2008". Multiple government agencies had acted to cut the number of Comanches on order, but, as a consequence of the heavy reductions to the numbers to be procured, the unit costs soared.
On 23 February 2004, the U.S. Army announced that the termination of the Comanche program, stating at the time that they had determined that the RAH-66 to already require numerous upgrades to be viable on the battlefield and that, instead, the Army was to direct the bulk of its rotary funding towards renovating its existing attack, utility, and reconnaissance helicopters, as well as to accelerate the development of unmanned aerial vehicles (UAVs), which could also perform the scouting role intended for the Comanche with less risk. Since the cancellation, both of the prototypes have been placed on public display.
Origins and LHXEdit
During 1982, the U.S. Army initiated the Light Helicopter Experimental (LHX) program with the aim of producing a replacement for several existing rotorcraft, including the UH-1, AH-1, OH-6, and OH-58 helicopters. It was a further six years until, during 1988, a formal request for proposal (RFP) was issued to various manufacturers, in time which the requirement had evolved into a battlefield reconnaissance helicopter. During October 1988, it was revealed that two separate teams, these being Boeing–Sikorsky and Bell–McDonnell Douglas, received contracts to proceed with further development work upon their submitted concepts. During the 1990s, it was announced that the program's name had been changed from LHX to simply Light Helicopter (LH). During April 1991, the U.S. Army decided to select the design proposal produced by the Boeing–Sikorsky team as the contest winner; shortly thereafter, the team received a contract for the construction of four prototypes, which were intended to be operated in an extended demonstration and evaluation phase. It was in that same month that the helicopter received its official designation, that being RAH-66 Comanche, issued by the U.S. Army.
During November 1993, assembly of the first prototype commenced at two separate locations, these being Sikorsky's facility in Stratford, Connecticut and Boeing's manufacturing plant in Philadelphia, Pennsylvania; later on, all of the rotorcraft's sub-assemblies were transferred to the former location where final assembly occurred. In the following year, the number of prototypes to be produced was reduced from four to two rotorcraft. On 25 May 1995, the first Comanche prototype was formally rolled out at Sikorsky's production facility, after which it was transferred to West Palm Beach, Florida to commence flight testing activities. On 4 January 1996, the prototype, flown by test pilots Bob Gradle and Rus Stiles, performed its 39-minute maiden flight. The first flight had been originally planned to take place during August 1995, but had been delayed by a number of structural and software problems that had been encountered. On 30 March 1999, the second prototype conducted its first flight, before joining the flight test program shortly thereafter.
The flight test program was conducted using the pair of prototypes produced, which had been assigned the serial numbers 94-0327 and 95-0001. Following a demonstration of its ability to meet certain key criteria, on 1 June 2000, it was announced that the RAH-66 had entered the $3.1 billion engineering and manufacturing development (EMD) phase of the program. Through the early 2000s, the U.S. Army maintained its plans for the intended purchase of over 1,200 Comanches, which were to fill both the scout helicopter and light attack roles; as late as 2003, it was being anticipated that deliveries of operational RAH-66s would commence as scheduled during 2006.
However, the program was not problem-free. During late 2000, it was revealed that an effort to reduce the Comanche's empty weight by approximately 200 lb (91 kg) or 2.1 per cent in order to conform with its established target weight had been initiated. The first Comanche prototype, serial 94-0327, completed 318 flights over 387 hours before reaching the end of its testing career during January 2002. The second prototype, serial 95-0001, had accumulated 103.5 flight hours and 93 sorties by May 2001. During late 2001 and early 2002, testing with the second RAH-66 was halted while the aircraft underwent extensive modifications, received both mission equipment and more powerful T800-LHT-801 engines. On 23 May 2002, the second prototype re-commenced flight testing with the additional equipment fitted. Accordingly, the expanded test programme involved new aspects such as the testing of the armaments and night vision systems; these test flights continued into 2003. During testing, the Comanche was recorded as having attained a cruise speed of 162 knots (186 mph; 300 km/h), as well as having achieved a "dash speed" of 172 knots (198 mph; 319 km/h); perhaps one of its more atypical capabilities was the demonstrated ability to perform a 180° turn in under five seconds.
During 2002, the Comanche program underwent heavy restructuring; consequently, the number of Comanches that were intended to be purchased was dropped down to 650 rotorcraft. At the time, the projected total cost for the full production of the Comanche in such numbers stood at $26.9 billion. Originally, the EMD phase had been planned to last for six years, as well as having involved a total of five Comanches being constructed to participate in the testing regime. During 2003, production on the third RAH-66, which was intended to be the first EMD-conformant helicopter, was started. Subsequently, eight RAH-66s were to be constructed for operational testing purposes. As planned, the initial production RAH-66s were to be completed to a Block I configuration, which would have included the majority of the rotorcraft's planned weapons and sensors. From the 16th Comanche onwards, deliveries would have been made to the Block II standard, which was to have all of the planned capabilities included.
On 23 February 2004, the U.S. Army announced that they had decided to terminate all work on the Comanche program. At the time, it was stated that the Army had determined that a number of upgrades would be necessary in order for the RAH-66 to be capable of surviving on the battlefield in the face of current anti-aircraft threats; however, the Army had instead decided to re-direct the bulk of its funding for rotary development toward the renovation of its existing helicopter fleet of attack, utility, and reconnaissance aircraft. Specifically, the Army also had plans to reuse the funds allocated to the Comanche program to speed up development of unmanned aerial vehicles (UAVs), which could also perform the scouting role intended for the vehicle. At the time of its termination, the Comanche program had reportedly spent US$6.9 billion. The contract termination fees involved were estimated to total US$450–680 million for the main program partners Sikorsky and Boeing.
Subsequently, the Army decided to pursue development of another battlefield scout helicopter under the Armed Reconnaissance Helicopter program; this resulted in another rotorcraft, designated as the Bell ARH-70, being selected and developed with the intention to replace the OH-58D in place of the Comanche. However, during October 2008, it was announced that the ARH-70 also met with cancellation, reportedly due to cost overruns on its development.
A multitude of reasons contributed to the ultimate cancellation of the RAH-66 program. According to aviation author James Williams, efforts to speed up the program via the elimination of risk-mitigation measures and the stream of continuous adjustments to account for annual budget cuts to the rotorcraft resulted in the formation of a negative cycle that functioned to greatly extend the rotorcraft's development schedule. Over the course of the Comanche's development, multiple government agencies had acted to cut the number of helicopters that were intended to be ordered; one particularly common basis for such curtailments was that the Cold War had ended and thus such quantities were unnecessary (a phenomenon known as the "Peace Dividend"). However, significant reductions in volume directly resulted in the rapid climbs in the projections of the Comanche's unit cost; in turn, this stimulated and gave validity to critics of the program, such as the Army Acquisition Executive James Ambrose, who had prominently declared that the Army would not receive any aircraft "costing a dollar over $7.5 million".
As early as 1995, it is claimed by Williams that the Comanche had been facing complete cancellation as a choice between which defense development programs were to be scrapped. During mid-1999, the Comanche was subject to substantial governmental scrutiny; the Government Accountability Office (GAO) reported that it had "serious doubts" about the program and noted that the Comanche would "consume almost two thirds of the whole Aviation budget by Fiscal Year 2008". In addition, wartime experiences, such as from the Kosovo War, had led to some senior figures within the Army to place a greater emphasis on the use of unmanned platforms for conducting many of the same roles for which the Comanche was being developed to perform. By 2000, Williams postulates that the primary reason for retaining the program was out of concern for the state of the helicopter industry—Sikorsky's production and employment figures were at their lowest for decades and the contract was considered critical.
Author Fred Brooks criticized the program's requirement for the Comanche to be capable of ferrying itself across the Atlantic as an example of excessive requirements being present in a project's design phase and of their costly repercussions. Williams observes that the Comanche's weight requirements were unachievable, and claimed that this was due to poor management, in which no party was allegedly aware of or in control of the rotorcraft's final weight; there were concerns that, when outfitted with actual equipment required for operations, the Comanche's engines would be incapable of lifting the total weight of the helicopter. Additionally, it has been claimed that it proved difficult to convince the Army that the program suffered from serious troubles while key individuals failed to realize the existence of insurmountable technical problems. Prized elements of the program, such as certain software capabilities and its integration, failed to foster confidence with Army overseers; several capabilities were viewed as having been unproven and risky, while the anticipated consumption of up to 40 per cent of the aviation budget by the Comanche alone for a number of years was considered to be extreme. According to Williams, it was concluded that the Army's aviation budget would be better spent on the delivery of less risky and more critical needs.
In a report published during 2008, the GAO recorded that an Army spokesperson had stated that "the program's costs could no longer be justified". Author Cindy Williams stated of the Comanche: "The rationale for cutting Comanche... is twofold. First, the doctrinal niche that the Comanche occupies is unnecessary in the near term and probably not viable in the longer term. Secondly, as with all rotary-wing aircraft, the Comanche is a voracious consumer of strategic airlift."
The manufacturing team, Sikorsky and Boeing, have attributed factors that were outside of their control, such as budget cuts, "requirement creep," and a protracted development period, to have caused problems with the program, rather than dysfunctionality on their part. Under the Comanche program, each company was responsible for the construction of different elements of the rotorcraft. Since the termination, both companies have decided to team up again to produce a jointly-developed prototype, designated as the SB-1 Defiant, for the Army's Future Vertical Lift (FVL) programme.
The Boeing–Sikorsky RAH-66 Comanche was intended to be an advanced five-blade armed reconnaissance and attack helicopter. The Comanche was specifically tailored to the role of armed scout to replace the U.S. Army's OH-58D Kiowa Warrior, which is an upgraded version of a Vietnam War-era observation helicopter. It was both smaller and lighter than the AH-64 Apache attack helicopter that it had been intended to accompany. The RAH-66 was powered by a pair of LHTEC T800 turboshaft engines, each capable of generating up to 1,563 hp (1,165 kW) of power. The RAH-66's fuselage was 43 feet (13 m) long and composed of composite materials; it was designed to be capable of fitting more readily onto transport ships, enabling the Comanche to be more rapidly deployed to flash points and other rapidly-developing situations. However, in the event of strategic transport assets not being available, the rotorcraft's ferry range of 1,200 nmi (2,200 km) would have allowed it to fly itself to battlefields overseas on its own.
As intended, it would have functioned as a stealth helicopter, incorporating a number of different techniques and technologies in order to reduce its radar cross-section (RCS) along with other areas of visibility and detectability. The exterior surfaces of the RAH-66 were faceted and covered with both radar-absorbent material (RAM) coatings and infrared-suppressant paint; as a result of these combined measures, the Comanche's RCS was stated to be 360 times smaller than that of the AH-64 Apache attack helicopter. The acoustic signature of the rotorcraft was also reported to be noticeably lower than comparative helicopters; this reduction had been partially achieved through the adoption of an all-composite five-blade main rotor and pioneering canted tail rotor assembly.
As intended, the Comanche was to be equipped with sophisticated avionics, including navigation and detection systems, which would have enabled operations during nighttime and within challenging weather conditions. Its primary mission was to scout around using its advanced sensors, attempting to find and designate targets for attack helicopters, such as the AH-64 Apache, to strike. The Comanche was furnished with a digital fly-by-wire flight control system. Each of the two crew members were to be provided with a pair of LCD multi-functional displays which would have functioned in addition to the Helmet-Integrated Display and Sight System (HIDSS) worn by the crew.
For the light attack role, the RAH-66 was to be furnished with various armaments. It was equipped with a single 20 mm three-barrel XM301 rotary cannon, which was mounted to the fuselage under the cockpit. In addition, the RAH-66 was capable of internally carrying a maximum of six AGM-114 Hellfire air-to-ground missiles or up to twelve AIM-92 Stinger air-to-air missiles, which would be evenly divided between a pair of retractable weapons pylons. Beyond storing munitions internally, the Comanche could also carry up to four Hellfire missiles or a maximum of eight Stinger missiles externally on each of its stub wings. However, operations performing with armaments mounted externally would reduce of the effectiveness of the rotorcraft's stealth technologies.
Aircraft on displayEdit
- Crew: two
- Length: 46.85 ft (14.28 m)
- Rotor diameter: 39.04 ft (11.90 m)
- Height: 11.06 ft (3.37 m)
- Disc area: 1,197 ft² (111 m²)
- Empty weight: 9,300 lb (4,218 kg)
- Useful load: 5,062 lb (2,296 kg)
- Loaded weight: 12,349 lb (5,601 kg)
- Max. takeoff weight: 17,408 lb (7,896 kg)
- Fuselage length: 43.31 ft (13.20 m)
- Rotor systems: 5-bladed main rotor, 8-bladed fan-in-fin anti-torque system (FANTAIL)
- Powerplant: 2 × LHTEC T800-LHT-801 turboshaft, 1,563 hp (1,165 kW) each
- Maximum speed: 175 knots (201 mph, 324 km/h)
- Cruise speed: 165 knots (190 mph, 306 km/h)
- Range: 262 nmi (302 mi, 485 km) on internal fuel
- Combat radius: 150 nmi (173 mi, 278 km) on internal fuel
- Ferry range: 1,200 nmi (1,380 mi, 2,220 km)
- Endurance: 2.5 hr
- Service ceiling: 14,980 ft (4,566 m)
- Rate of climb: 895 ft/min (4.55 m/s)
- Disc loading: 10.32 lb/ft² (50.4 kg/m2)
- 1× 20 mm XM301 three-barrel rotary cannon mounted in a Turreted Gun System (capacity: 500 rounds)
- Internal bays: 6× AGM-114 Hellfire air-to-ground missiles, or 12× AIM-92 Stinger air-to-air missiles, or 24× 2.75 in (70 mm) Hydra 70 air-to-ground rockets
- Optional stub wings: 8× Hellfires, 16× Stingers, or 56× Hydra 70 rockets
Aircraft of comparable role, configuration and era
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