|Three view of a Boeing 2707-300|
|National origin||United States|
|Manufacturer||Boeing Commercial Airplanes|
The Boeing 2707 was the first American supersonic transport (SST) project. After winning a competition for a government-funded contract to build an American SST, Boeing began development at its facilities in Seattle, Washington. The design emerged as a large aircraft with seating for 250 to 300 passengers and cruise speeds of approximately Mach 3. It would have been much larger and faster than preceding SST designs such as Concorde.
The SST was the topic of considerable concern within and outside the aviation industry. From the start, the airline industry had noted that the economics of the design were questionable, concerns that were only partially addressed during development. Outside the field, the entire SST concept was the subject of considerable negative press, centered on the issue of sonic booms and effects on the ozone layer.
A key design feature of the 2707 was its use of a swing wing configuration. During development the required weight and size of this mechanism continued to grow, forcing the team to start over using a conventional delta wing. Rising costs and the lack of a clear market led to its cancellation in 1971 before two prototypes had been completed.
Boeing had worked on a number of small-scale SST studies since 1952. In 1958, it established a permanent research committee, which grew to a $1 million effort by 1960. The committee proposed a variety of alternative designs, all under the name Model 733. Most of the designs featured a large delta wing, but in 1959 another design was offered as an offshoot of Boeing's efforts in the swing-wing TFX project (which led to the purchase of the General Dynamics F-111 instead of the Boeing offering). In 1960, an internal "competition" was run on a baseline 150-seat aircraft for trans-Atlantic routes, and the swing-wing version won.
Shortly after taking office, President John F. Kennedy tasked the Federal Aviation Administration with preparing a report on "national aviation goals for the period between now and 1970". The study was prompted in the wake of several accidents, which led to the belief that the industry was becoming moribund. Two projects were started, Project Beacon on new navigational systems and air traffic control, and Project Horizon on advanced civil aviation developments.
Only one month later the FAA's new director, Najeeb Halaby, produced the Commission on National Aviation Goals, better known as Project Horizon. Among other suggestions, the report was used as a platform to promote the SST. Halaby argued that a failure to enter this market would be a "stunning setback". The report was met by skepticism by most others. Kennedy had put Lyndon Johnson on the SST file, and he turned to Robert McNamara for guidance. McNamara was highly skeptical of the SST project and savaged Halaby's predictions; he was also afraid the project might be turned over to the DoD and was careful to press for further studies.
The basic concept behind the SST was that its fast flight would allow them to fly more trips than a subsonic aircraft, leading to higher utilization. However, it did this at the cost of greatly increased fuel use. If fuel costs were to change dramatically, SSTs would not be competitive. These problems were well understood within the industry; the IATA released a set of "design imperatives" for an SST that were essentially impossible to meet—the release was a warning to promoters of the SST within the industry.
By mid-1962, it was becoming clear that tentative talks earlier that year between the British Aircraft Corporation and Sud Aviation on a merger of their SST projects were more serious than originally thought. In November 1962, still to the surprise of many, the Concorde project was announced. In spite of marginal economics, nationalistic and political arguments had led to wide support for the project, especially from Charles de Gaulle. This set off something of a wave of panic in other countries, as it was widely believed that almost all future commercial aircraft would be supersonic, and it looked like the Europeans would start off with a huge lead. As if this weren't enough, it soon became known that the Soviets were also working on a similar design.
Three days after the Concorde announcement, Halaby wrote a letter to Kennedy suggesting that if they did not immediately start their own SST effort, the US would lose 50,000 jobs, $4 billion in income, and $3 billion in capital as local carriers turned to foreign suppliers. A report from the Supersonic Transport Advisory Group (STAG) followed, noting that the European team was in the lead in basic development, and suggested competing by developing a more advanced design with better economics. At the time, more advanced generally meant higher speed. The baseline design in the report called for an aircraft with Mach 3 performance with 2,400 mile range in order to serve the domestic market. They felt that there was no way to build a transatlantic design with that performance in time to catch the Concorde's introduction, abandoning the trans-Atlantic market to the Europeans.
In spite of vocal opponents, questions about the technical requirements, and extremely negative reports about its economic viability, the SST project gathered strong backing from industry and the FAA. Johnson sent a report to the president asking for $100 million in funding for FY64. This might have been delayed, but in May, Pan Am announced they had placed options on the Concorde. Juan Trippe leaked the information earlier that month, stating that the airline would not ignore the SST market, and would buy from Europe if need be.
Requests for Proposals were sent out to airframe manufacturers Boeing, Lockheed, and North American for the airframes; and Curtiss-Wright, General Electric and Pratt & Whitney for engines. The FAA estimated that there would be a market for 500 SSTs by 1990. In spite of not having even a selected design, orders from air carriers started flowing in immediately. Preliminary designs were submitted to the FAA on January 15, 1964.
Boeing's entry was essentially identical to the swing-wing Model 733 studied in 1960; it was known officially as the Model 733-197, but also referred to both as the 1966 Model and the Model 2707. The latter name became the best known in public, while Boeing continued to use 733 model numbers internally. The design resembled the future B-1 Lancer bomber, with the exception that the four engines were mounted in individual nacelles instead of pairs on the Lancer. The blended wing root spanned almost all of cabin area, and this early version had a much more stubby look than the models that would ultimately evolve. The wing featured extensive high-lift devices on both the leading and trailing edges, minimizing the thrust required, and thus noise created, during climb out. The proposal also included optional fuselage stretches that increased capacity from the normal 150 seats to 227.
Lockheed's entry, designated CL-823, was essentially an enlarged Concorde. Like the Concorde, it featured a long and skinny fuselage, engines under the wing, and a compound delta planform. The only major design difference was the use of individual pods for the engines, rather than pairs. The CL-823 lacked any form of high-lift devices on the wings, relying on engine power and long runways for liftoff, ensuring a huge noise footprint. The CL-823 was the largest of the first-round entries, with typical seating for 218.
The North American NAC-60 was essentially a scaled-up B-70 with a less tapered fuselage and new compound-delta wing. The design retained the high-mounted canard above the cockpit area, and the box-like engine area under the fuselage. The use of high-lift devices on the leading edge of the wing lowered the landing angles to the point where the "drooping nose" was not required, and a more conventional rounded design was used. Compared to the other designs, the rounded nose profile and more cylindrical cross-section gave the NAC-60 a decidedly more conventional look than the other entries. This also meant it would fly slower, at Mach 2.65.
A "downselect" of the proposed models resulted in the NAC-60 and Curtiss-Wright efforts being dropped from the program, with both Boeing and Lockheed asked to offer SST models meeting the more demanding FAA requirements and able to use either of the remaining engine designs from GE or P&W. In November, another design review was held, and by this time Boeing had scaled up the original design into a 250-seat model, the Model 733-290. Due to concerns about jet blast, the four engines were moved to a position underneath an enlarged tailplane. When the wings were in their swept-back position, they merged with the tailplane to produce a delta-wing planform.
Both companies were now asked for considerably more detailed proposals, to be presented for final selection in 1966. When this occurred, Boeing's design was now the 300-seat Model 733-390. Both the Boeing and Lockheed L-2000 designs were presented in September 1966 along with full-scale mock-ups. After a lengthy review the Boeing design was announced as the winner on January 1, 1967. The design would be powered by the General Electric GE4/J5 engines. Lockheed's L-2000 was judged simpler to produce and less risky, but its performance was slightly lower and its noise levels slightly higher.
Refining the design
The 733-390 would have been an advanced aircraft even if it had been only subsonic. It was one of the earliest wide-body aircraft designs, with 2-3-2 row seating arrangement at its widest section in a fuselage that was considerably wider than aircraft then in service. The SST mock-up included both overhead storage for smaller items with restraining nets, as well as large drop-in bins between sections of the aircraft. In the main 247-seat tourist-class cabin, the entertainment system consisted of retractable televisions placed between every sixth row in the overhead storage. In the 30-seat first-class area, every pair of seats included smaller televisions in a console between the seats. Windows were only 6 inches due to the high altitudes the aircraft flew at maximizing the pressure on them, but the internal pane was 12" to give an illusion of size.
Boeing predicted that if the go-ahead were given, construction of the SST prototypes would begin in early 1967 and the first flight could be made in early 1970. Production aircraft could start being built in early 1969, with the flight testing in late 1972 and certification by mid-1974.
A major change in the design came when Boeing added canards behind the nose—which added weight. Boeing also faced insurmountable weight problems due to the swing-wing mechanism (a titanium pivot section having been fabricated with a weight of 4,600 pounds and measuring eleven feet long and 2.5 feet thick) and the design could not achieve sufficient range. Flexing of the fuselage (it would have been the longest ever built) threatened to make control difficult. In October 1968, the company was finally forced to abandon the variable geometry wing. The Boeing team fell back on a tailed delta fixed wing. The new design was also smaller, seating 234, and known as the Model 2707-300. Work began on a full-sized mock-up and two prototypes in September 1969, now two years behind schedule.
A promotional film claimed that airlines would soon pay back the federal investment in the project, and it was projected that SSTs would dominate the skies with subsonic jumbo jets (such as Boeing's own 747) being only a passing intermediate fad.
By October 1969, there were delivery positions reserved for 122 Boeing SSTs by 26 airlines, including Alitalia, Canadian Pacific Airlines, Delta Air Lines, Iberia, KLM, Northwest Airlines, and World Airways.
By this point, the opposition to the project was becoming increasingly vocal. Environmentalists were the most influential group, voicing concerns about possible depletion of the ozone layer due to the high altitude flights, and about noise at airports and from sonic booms.
The latter became the most significant rallying point, especially after the publication of the anti-SST paperback, "SST and Sonic Boom Handbook" edited by William Shurcliff, which claimed that a single flight would "leave a 'bang-zone' 50 miles wide by 2,000 miles long" along with a host of associated problems. In tests in 1964 with the XB-70 near Oklahoma City, the path had a maximum width of 16 miles, but still resulted in 9,594 complaints of damage to buildings, 4,629 formal damage claims, and 229 claims for a total of $12,845.32, mostly for broken glass and cracked plaster. As the opposition widened, the claimed negative effects became ever odder, including upsetting people who do delicate work (e.g., brain surgeons), harming persons with nervous ailments, and even inducing miscarriages.
Other concerns were also added to the list, although the evidence for them was essentially non-existent. One was that the water vapor released by the engines into the stratosphere would envelop the earth in a "global gloom". Presidential Adviser Russell Train warned that a fleet of 500 SSTs flying at 65,000 ft. for a period of years could raise stratospheric water content by as much as 50% to 100%. According to Train, this could lead to greater ground-level heat and hamper the formation of ozone. Later, an additional threat to the ozone was found in the exhaust's nitrogen oxides, a threat that was later validated by MIT. More recent analysis in 1995 by David W. Fahey, an atmospheric scientist at the National Oceanic and Atmospheric Administration, and others found that the drop in ozone would be from 1 to 2% if a fleet of 500 supersonic aircraft was operated. Fahey expressed the opinion that this would not be a fatal obstacle for an advanced SST development.
During the 1970s the alleged potential for serious ozone damage and the sonic boom worries were picked up by the Sierra Club, the National Wildlife Federation and the Wilderness Society. Supersonic flight over land in the United States was eventually banned, and several states added additional restrictions or banned Concorde outright.
Senator William Proxmire (D-Wisconsin) criticized the SST program as frivolous federal spending. Ultimately, supersonic passenger service was not economically competitive, and ceased with the retirement of Concorde in 2003; as of 2015, no commercial supersonic aircraft operate in the world, due largely to poor fuel economy and high maintenance costs.
Halaby attempted to dismiss these concerns, stating "The supersonics are coming−as surely as tomorrow. You will be flying one version or another by 1980 and be trying to remember what the great debate was all about."
Government funding cut
In March 1971, despite the project's strong support by the administration of President Richard Nixon, the U.S. Senate rejected further funding. A counterattack was organized under the banner of the "National Committee for an American SST", which urged supporters to send in $1 to keep the program alive. Afterward, letters of support from aviation buffs, containing nearly $1 million worth of contributions, poured in. Labor unions also supported the SST project, worried that the winding down of both the Vietnam War and Apollo program would lead to mass unemployment in the aviation sector. AFL-CIO President George Meany suggested that the race to develop a first-generation SST was already lost, but the US should "enter the competition for the second generation —the SSTs of the 1980s and 1990s."
In spite of this newfound support, the House of Representatives also voted to end SST funding on 20 May 1971. The vote was highly contentious. Gerald Ford, then Republican Leader, shouted Meany's claims that "If you vote for the SST, you are ensuring 13,000 jobs today plus 50,000 jobs in the second tier and 150,000 jobs each year over the next ten years." Sidney Yates, leading the "no" camp, demanded a public vote (at that time a newly introduced procedure) and eventually won the vote against further funding, 215 to 204.
At the time, there were 115 unfilled orders by 25 airlines, while Concorde had 74 orders from 16 customers. The two prototypes were never completed. Due to the loss of several government contracts and a downturn in the civilian aviation market, Boeing reduced its number of employees by more than 60,000. The SST became known as "the airplane that almost ate Seattle." As a result of the mass layoffs and so many people moving away from the city in search of work, a billboard was erected near Sea-Tac airport in 1971 that read, "Will the last person leaving Seattle - turn out the lights".
When the Concorde launched, predicted sales were 150; in the event, only 14 airframes were built for commercial service. Service entry was only secured through large government funding subsidy. These few aircraft went on to have a very long in-service flight and were ultimately commercially successful for its operators, until finally removed from service in the aftermath of the 9/11 terrorist attacks when Airbus decided to end servicing arrangements.
With the ending of the 2707 project, the entire SST field in the U.S. was moribund for some time. By the mid-1970s, minor advances, combined, appeared to offer greatly improved performance. Through the second half of the 1970s, NASA provided funding for the Advanced Supersonic Transport (AST) project at several companies, including McDonnell Douglas, Boeing, and Lockheed. Considerable wind tunnel testing of the various models was carried out at NASA's Langley Research Center.
Though many designs have been studied since, it is unlikely SST aircraft will be economically feasible in the foreseeable future. The inherent lower lift-to-drag ratios at supersonic speeds mean SSTs will have poorer fuel economy than subsonic designs. Even faster subsonic designs, like the Boeing Sonic Cruiser, have been met with little industry interest in an era of increasingly difficult economic pressures on the airlines.
Nevertheless, the SST race has had several lasting effects on the industry as a whole. The supercritical wing was originally developed as part of the SST efforts in the U.S., but is now widely used on most jet aircraft. In Europe, the cooperation that allowed the Concorde led to the formation of Airbus, Boeing's foremost competitor.
The Museum of Flight in Seattle parks its Concorde a few blocks from the building where the original 2707 mockup was housed in Seattle. While the Soviet Tu-144 had a short service life, Concorde was successful enough to fly as a small luxury fleet from 1976 until 2003, for the most part highly profitable for the airlines in the niche transatlantic market. As the most advanced supersonic transports became some of the oldest airframes in the fleet, profits eventually fell, due to rising maintenance costs.
The final-configuration mockup was sold to a museum and displayed at the SST Aviation Exhibit Center in Kissimmee, Florida from 1973 to 1981. In 1983, the building, complete with SST, was purchased by the Faith World church. For years the Osceola New Life Assembly of God held services there with the airplane still standing above. In 1990, the mock-up was sold to aircraft restorer Charles Bell, who moved it, in pieces, to Merritt Island, in order to preserve it while it waited for a new home as the church now wanted the space for expansion. The forward fuselage was on display at the Hiller Aviation Museum of San Carlos, California for many years, but in early 2013, was moved back to Seattle, where it is undergoing restoration at the Museum of Flight.
|Line drawings of variants|
- Variable sweep wing
- Same as -100, but with canards
- Stationary wing
Specifications (Boeing 2707-200)
Data from
- Capacity: 277 passengers
- Payload: 75,000 lb (34,000 kg) maximum
- Length: 306 ft (93.27 m)
- Wingspan: 180 feet 4 inches (54.97 m) spread
105 feet 9 inches (32.23 m) swept ()
- Height: 46 ft 3 in (14.10 m)
- Empty weight: 287,500 pounds (130,400 kg) (International model)
- Loaded weight: 675,000 pounds (306,000 kg) (maximum ramp weight)
- Max. landing weight: 430,000 pounds (200,000 kg)
- Powerplant: 4 × General Electric GE4/J5P turbojets, 63,200 lbf (281 kN) (with augmentation) each
- Cruise speed: Mach 2.7: 1,800 miles per hour (2,900 km/h)
- Range: 4,250 mi (7,871 km) with 277 passengers
- Takeoff length: 5,700 feet (1,700 m)
Landing length: 6,500 feet (2,000 m)
- Planes That Never Flew, Discovery Channel
- Aircraft of comparable role, configuration and era
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- Conway, p. 75.
- Conway, p. 78.
- Lt Col Donald I. Hackney. "The Supersonic Transport as an Instrument of National Power"[permanent dead link]. US Army War College, 8 April 1966
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|Wikimedia Commons has media related to Boeing 2707.|
- NASA Innovation in Flight — NASA monograph covering projects from B-70 to Boeing and Lockheed SST designs and recent SST studies
- Boeing Supersonic Transport page
- Boeing 2707-300 on Vectorsite.net
- Boeing SST on Super70s.com
- Boeing SST mockup on display at the Hiller Aviation Museum
- 1964 Concept Film at British Movietone Digital Archive
- "Ticket Through The Sound Barrier" - 1966 Supersonic Transport Educational Documentary
- Boeing 2707-300 Description at emotionreports.com
- Initial 733 proposal images on Russian site sergib.agava.ru
- "The United States SST Contenders" a 1964 Flight article
- "The Boeing SST Could Operate with ... an advertisement for the proposed Boeing Model 733-390 in Flight, 1965.
- Boeing's latest SST proposal. Part 1. Flight, 1969.
- Boeing's latest SST proposal. Part 2. Flight, 1969.