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138-466: John D. Odegard (1941–1998) started the program in 1968 with only two donated aircraft and one other faculty member besides himself. Over time, the program was able to purchase more aircraft and grew dramatically in the number of students enrolled. In 1982, the Center for Aerospace Sciences was established as a result of the growth of UND’s atmospheric research and aviation education programs. In 1997, as part of

276-514: A May 1978 crash , while a potential competitor, the Boeing 2707 , was cancelled in 1971 before any prototypes were built. On 25 July 2000, Air France Flight 4590 crashed shortly after take-off with all 109 occupants and four on the ground killed. This was the only fatal incident involving Concorde; commercial service was suspended until November 2001. The surviving aircraft were retired in 2003, 27 years after commercial operations had begun. All but 2 of

414-550: A Supplemental Type Certificate that allowed the installation of Garmin Avionics G500H suite. UND Aerospace is the current holder for the STC. Having updated avionics allows student to train from Private pilot, Instrument, Commercial, CFI and CFII in the same airframe. In January 2017 UND Aerospace took delivery of a Robinson R44 Cadet. Equipped with Garmin G500H, GTN 750, and GTX345 it

552-460: A balloon carrier (the precursor to the aircraft carrier ) in the first offensive use of air power in naval aviation . Austrian forces besieging Venice attempted to launch some 200 incendiary balloons at the besieged city. The balloons were launched mainly from land; however, some were also launched from the Austrian ship SMS  Vulcano . At least one bomb fell in the city; however, due to

690-783: A drone , is an aircraft with no human pilot , crew, or passengers on board. UAVs were originally developed through the twentieth century for military missions too "dull, dirty or dangerous" for humans, and by the twenty-first, they had become essential assets to most militaries. As control technologies improved and costs fell, their use expanded to many non-military applications. These include aerial photography , area coverage, precision agriculture , forest fire monitoring, river monitoring, environmental monitoring , policing and surveillance, infrastructure inspections, smuggling, product deliveries , entertainment, and drone racing . Many terms are used for aircraft which fly without any persons on board. The term drone has been used from

828-490: A "powered, aerial vehicle that does not carry a human operator, uses aerodynamic forces to provide vehicle lift, can fly autonomously or be piloted remotely, can be expendable or recoverable, and can carry a lethal or nonlethal payload". UAV is a term that is commonly applied to military use cases. Missiles with warheads are generally not considered UAVs because the vehicle itself is a munition, but certain types of propeller-based missile are often called " kamikaze drones " by

966-566: A 30th anniversary celebration, the school took on its present name in honor of its founder. The founder of the aviation program at UND, John D. Odegard, logged over 10,000 hours of flight time in his life and was licensed for commercial flight and instrument operations. He was type-rated in Cessna Citations, Learjet, and Beechjet, as well as being a certificated flight instructor (CFI) and certified examiner for commercial, instrument, tailwheel, multiengine, and Citation type-ratings. Having broken

1104-410: A British design (as they had on the earlier subsonic Caravelle ). As neither company had experience in the use of heat-resistant metals for airframes, a maximum speed of around Mach 2 was selected so aluminium could be used – above this speed, the friction with the air heats the metal so much that it begins to soften. This lower speed would also speed development and allow their design to fly before

1242-503: A European company, and the risk of "giving away" US technological leadership to a European partner. When the STAC plans were presented to the UK cabinet, the economic considerations were considered highly questionable, especially as these were based on development costs, now estimated to be £ 150 million ( US$ 420 million), which were repeatedly overrun in the industry. The Treasury Ministry presented

1380-591: A Scotsman claiming, "you talk about 'E' for England, but part of it is made in Scotland." Given Scotland's contribution of providing the nose cone for the aircraft, Benn replied, "it was also 'E' for 'Écosse' (the French name for Scotland) – and I might have added 'e' for extravagance and 'e' for escalation as well!" In common usage in the United Kingdom, the type is known as "Concorde" without an article , rather than "

1518-441: A camera) that weigh considerably less than an adult human, and as a result, can be considerably smaller. Though they carry heavy payloads, weaponized military UAVs are lighter than their crewed counterparts with comparable armaments. Small civilian UAVs have no life-critical systems , and can thus be built out of lighter but less sturdy materials and shapes, and can use less robustly tested electronic control systems. For small UAVs,

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1656-498: A change in the public opinion of SSTs. By 1976 the remaining buyers were from four countries: Britain, France, China, and Iran. Only Air France and British Airways (the successor to BOAC) took up their orders, with the two governments taking a cut of any profits. The US government cut federal funding for the Boeing 2707 , its supersonic transport programme, in 1971; Boeing did not complete its two 2707 prototypes. The US, India, and Malaysia all ruled out Concorde supersonic flights over

1794-469: A clause, originally asked for by the UK government, imposing heavy penalties for cancellation. This treaty was signed on 29 November 1962. Charles de Gaulle vetoed the UK's entry into the European Community in a speech on 25 January 1963. At Charles de Gaulle's January 1963 press conference the aircraft was first called 'Concorde'. The name was suggested by the eighteen-year-old son of F.G. Clark,

1932-574: A component of an unmanned aircraft system ( UAS ), which also includes a ground-based controller and a system of communications with the aircraft. The term UAS was adopted by the United States Department of Defense (DoD) and the United States Federal Aviation Administration (FAA) in 2005 according to their Unmanned Aircraft System Roadmap 2005–2030. The International Civil Aviation Organization (ICAO) and

2070-412: A delta wing running most of the length of the fuselage, this was no longer easy; moving the wing would leave it in front of the nose or behind the tail. Studying the various layouts in terms of CG changes, both during design and changes due to fuel use during flight, the ogee planform immediately came to the fore. To test the new wing, NASA assisted the team by modifying a Douglas F5D Skylancer to mimic

2208-525: A digital processor for intake control. It was the first use of a digital processor with full authority control of an essential system in a passenger aircraft. It was developed by BAC's Electronics and Space Systems division after the analogue AICUs (developed by Ultra Electronics ) fitted to the prototype aircraft were found to lack sufficient accuracy. Ultra Electronics also developed Concorde's thrust-by-wire engine control system. Engine failure causes problems on conventional subsonic aircraft ; not only does

2346-419: A dump door, an auxiliary inlet and a ramp bleed to the exhaust nozzle. As well as supplying air to the engine, the intake also supplied air through the ramp bleed to the propelling nozzle. The nozzle ejector (or aerodynamic) design, with variable exit area and secondary flow from the intake, contributed to good expansion efficiency from take-off to cruise. Concorde's Air Intake Control Units (AICUs) made use of

2484-410: A host of advanced technologies that allow them to carry out their missions without human intervention, such as cloud computing, computer vision, artificial intelligence, machine learning, deep learning, and thermal sensors. For recreational uses, an aerial photography drone is an aircraft that has first-person video, autonomous capabilities, or both. An unmanned aerial vehicle ( UAV ) is defined as

2622-413: A human operator, as remotely piloted aircraft ( RPA ), or with various degrees of autonomy , such as autopilot assistance, up to fully autonomous aircraft that have no provision for human intervention. Based on the altitude, the following UAV classifications have been used at industry events such as ParcAberporth Unmanned Systems forum: An example of classification based on the composite criteria

2760-801: A human target in Libya , according to a report from the UN Security Council 's Panel of Experts on Libya, published in March 2021. This may have been the first time an autonomous killer-robot armed with lethal weaponry attacked human beings. Superior drone technology, specifically the Turkish Bayraktar TB2 , played a role in Azerbaijan's successes in the 2020 Nagorno-Karabakh war against Armenia. UAVs are also used in NASA missions. The Ingenuity helicopter

2898-444: A layout would still have good supersonic performance, but also have reasonable take-off and landing speeds using vortex generation. The aircraft would have to take off and land very "nose high" to generate the required vortex lift , which led to questions about the low speed handling qualities of such a design. Küchemann presented the idea at a meeting where Morgan was also present. Test pilot Eric Brown recalls Morgan's reaction to

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3036-560: A negative view, suggesting that there was no way the project would have any positive financial returns for the government, especially in light that "the industry's past record of over-optimistic estimating (including the recent history of the TSR.2) suggests that it would be prudent to consider" the cost "to turn out much too low." This led to an independent review of the project by the Committee on Civil Scientific Research and Development, which met on

3174-493: A pair of air traffic control tower simulators. Finally, Ryan Hall is home to the remote classroom and several state of the art digital classrooms. The Grand Forks International Airport campus consists of the dispatch office where students request aircraft and are assigned to practice areas. The dispatch office opens out onto Bravo Ramp where the Seminoles, Cessnas, Decathlons, and some Archers are based. It also connects directly to

3312-436: A parallel increase in the use of drones for consumer and general aviation activities. As of 2021, quadcopter drones exemplify the widespread popularity of hobby radio-controlled aircraft and toys, however the use of UAVs in commercial and general aviation is limited by a lack of autonomy and by new regulatory environments which require line-of-sight contact with the pilot. In 2020, a Kargu 2 drone hunted down and attacked

3450-681: A particular route. This would remain economically advantageous as long as fuel represented a small percentage of operational costs. STAC suggested that two designs naturally fell out of their work, a transatlantic model flying at about Mach 2, and a shorter-range version flying at Mach 1.2. Morgan suggested that a 150-passenger transatlantic SST would cost about £75 to £90 million to develop, and be in service in 1970. The smaller 100-passenger short-range version would cost perhaps £50 to £80 million, and be ready for service in 1968. To meet this schedule, development would need to begin in 1960, with production contracts let in 1962. Morgan suggested that

3588-509: A perceived slight by de Gaulle. At the French roll-out in Toulouse in late 1967, the British Minister of Technology , Tony Benn , announced that he would change the spelling back to Concorde . This created a nationalist uproar that died down when Benn stated that the suffixed "e" represented "Excellence, England, Europe, and Entente (Cordiale) ". In his memoirs, he recounted a letter from

3726-518: A predominantly blue livery, with the exception of the wings, in a promotional deal with Pepsi . In this paint scheme, Air France was advised to remain at Mach 2 (2,120 km/h; 1,320 mph) for no more than 20 minutes at a time, but there was no restriction at speeds under Mach 1.7. F-BTSD was used because it was not scheduled for any long flights that required extended Mach 2 operations. UAV An unmanned aerial vehicle ( UAV ), or unmanned aircraft system ( UAS ), commonly known as

3864-512: A replacement of the earlier Piper PA-28 Warrior III fleet. UND Aerospace always tries to provide new, technologically advanced aircraft to its students. UND modified its fleet to include the Cessna 172 aircraft after Piper discontinued producing new Piper Warrior III's. UND later replaced the Cessna 172 fleet with the Piper Archer TX in 2016 as a part of their fleet renewal program. Rounding out

4002-519: A second King Air The school also was given a Piper PA-12 Supercruiser that was overhauled to provide students another aircraft to practice tailwheel landings. In April 2014, UND announced that it would begin phasing out their fleet of Cessna 172 Skyhawks in favor of the Piper Archer, marking a move back to the Piper Cherokee platform for UND's primary flight training. UND's first Piper Archer, N718ND,

4140-521: A similar aircraft after considering the SST problem and coming to the same conclusions as the Bristol and STAC teams in terms of economics. It was later revealed that the original STAC report, marked "For UK Eyes Only", had secretly been passed to France to win political favour. Sud made minor changes to the paper and presented it as their own work. France had no modern large jet engines and had already decided to buy

4278-527: A turbojet's noise could be reduced and SNECMA made advances in silencer design during the programme. The Olympus Mk.622 with reduced jet velocity was proposed to reduce the noise but was not pursued. By 1974, the spade silencers which projected into the exhaust were reported to be ineffective but "entry-into-service aircraft are likely to meet their noise guarantees". The powerplant configuration selected for Concorde highlighted airfield noise, boundary layer management and interactions between adjacent engines and

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4416-409: A twin-engined aircraft above Mach 1.6". Situated behind the wing leading edge, the engine intake had a wing boundary layer ahead of it. Two-thirds were diverted and the remaining third which entered the intake did not adversely affect the intake efficiency except during pushovers when the boundary layer thickened and caused surging. Wind tunnel testing helped define leading-edge modifications ahead of

4554-415: A variable payload are more likely to feature a distinct fuselage with a tail for stability, control and trim, although the wing configurations in use vary widely. For uses that require vertical flight or hovering, the tailless quadcopter requires a relatively simple control system and is common for smaller UAVs. Multirotor designs with 6 or more rotors is more common with larger UAVs, where redundancy

4692-406: A visor was used to keep high temperature air from flowing over the cockpit skin. Concorde had livery restrictions; the majority of the surface had to be covered with a highly reflective white paint to avoid overheating the aluminium structure due to heating effects. The white finish reduced the skin temperature by 6 to 11 °C (11 to 20 °F). In 1996, Air France briefly painted F-BTSD in

4830-552: A year. There is also a two-year program. Rex Ginder is the associate director in Phoenix. UND currently operates a fleet of 123 aircraft including 100 airplanes, 7 helicopters, and 9 unmanned aerial vehicles ( UAV's ). The majority of these aircraft are based at Grand Forks International Airport with the remainder located at the two satellite campuses in the United States. The fleet is primarily made up of 93 Piper Archer equipped with

4968-590: Is "Sioux". The University of North Dakota School of Aerospace Sciences is a member school of the National Intercollegiate Flying Association (NIFA). NIFA is a professional organization that provides a forum of competition and learning for aviation students from colleges all around the United States. In the fall of each year, UND Flying Team students participate in the Region V Safety and Flight Evaluation Conference (SAFECON). The regional SAFECON

5106-512: Is U.S. Military's unmanned aerial systems (UAS) classification of UAVs based on weight, maximum altitude and speed of the UAV component. UAVs can be classified based on their power or energy source, which significantly impacts their flight duration, range, and environmental impact. The main categories include: The earliest recorded use of an unmanned aerial vehicle for warfighting occurred in July 1849, with

5244-454: Is advantageous. The telephony designator (used instead of phonetically pronouncing the three letter company designator associated with the aircraft call sign) is usually assigned at the same time as the ICAO three letter designator. The call sign, together with a flight/trip number, is the aircraft identification for radio voice communications with air traffic personnel. The call sign for UND aircraft

5382-547: Is also less of a critical requirement for unmanned aircraft, allowing the designer greater freedom to experiment. Instead, UAVs are typically designed around their onboard payloads and their ground equipment. These factors have led to a great variety of airframe and motor configurations in UAVs. For conventional flight the flying wing and blended wing body offer light weight combined with low drag and stealth , and are popular configurations for many use cases. Larger types which carry

5520-468: Is an autonomous UAV that operated on Mars from 2021 to 2024. Current the Dragonfly spacecraft is being developed, and is aiming to reach and examine Saturn 's moon Titan . Its primary goal is to roam around the surface, expanding the amount of area to be researched previously seen by landers . As a UAV, Dragonfly allows examination of potentially diverse types of soil. The drone is set to launch in 2027, and

5658-458: Is estimated to take seven more years to reach the Saturnian system. Miniaturization is also supporting the development of small UAVs which can be used as individual system or in a fleet offering the possibility to survey large areas, in a relatively small amount of time. According to data from GlobalData , the global military uncrewed aerial systems (UAS) market, which forms a significant part of

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5796-472: Is hosted each year by one of the five member schools located in the adjacent states of Iowa, Minnesota, North Dakota, South Dakota and Wisconsin. Within Region V, the UND Flying Team consistently dominates the total School Ranking Overall calculated from the 13 various categories in which competition points are awarded. Likewise, a national SAFECON takes place in the spring season of the new year. Generally,

5934-630: Is ideally set up for SFAR transition training as well as Instrument and Instrument Instructor training. As of September 2011, the Unmanned Aircraft Systems (UAS) department employs nine aircraft for various missions including three CropCam, two Ravan, two Scan Eagle , one Draganflyer, and one Telemaster UAV's. Along with the aircraft, the university provides realistic ground training in UAV flying with its two Reaper, one Predator, and one Scan Eagle flight training devices (FTD). Past aircraft have included models from various manufactures. Prior to

6072-847: Is mostly utilized for storage and occasional regional law enforcement training. Clifford Hall houses the Atmospheric Sciences department, the Space Studies Department, the Department of Earth Systems Science & Policy, the UAS Center administrative offices, the Upper Midwest Aerospace Consortium, and the Scientific Computing Center. Dedicated in May 1992, it was the second addition to the aerospace complex on

6210-480: Is not available. 47°55′18″N 97°05′07″W  /  47.92167°N 97.08528°W  / 47.92167; -97.08528 Concorde Concorde ( / ˈ k ɒ ŋ k ɔːr d / ) is a retired Anglo-French supersonic airliner jointly developed and manufactured by Sud Aviation (later Aérospatiale ) and the British Aircraft Corporation (BAC). Studies started in 1954, and France and

6348-404: Is not generated the same way at supersonic and subsonic speeds, with the lift-to-drag ratio for supersonic designs being about half that of subsonic designs. The aircraft would need more thrust than a subsonic design of the same size. But although they would use more fuel in cruise, they would be able to fly more revenue-earning flights in a given time, so fewer aircraft would be needed to service

6486-481: Is prioritized. Traditional internal combustion and jet engines remain in use for drones requiring long range. However, for shorter-range missions electric power has almost entirely taken over. The distance record for a UAV (built from balsa wood and mylar skin) across the North Atlantic Ocean is held by a gasoline model airplane or UAV. Manard Hill "in 2003 when one of his creations flew 1,882 miles across

6624-461: Is the main building in the School of Aerospace Sciences complex on campus and was the first of the four buildings to be built. The building houses classrooms, a portion of faculty offices for the Department of Aviation, the main office of the School of Aerospace Sciences, a full-motion spatial disorientation simulator, an altitude chamber (used to teach flight students about the effects of high altitude on

6762-521: The 1991 Gulf War . UAVs demonstrated the possibility of cheaper, more capable fighting-machines, deployable without risk to aircrews. Initial generations primarily involved surveillance aircraft , but some carried armaments , such as the General Atomics MQ-1 Predator , that launched AGM-114 Hellfire air-to-ground missiles . CAPECON , a European Union project to develop UAVs, ran from 1 May 2002 to 31 December 2005. As of 2012 ,

6900-852: The Argus As 292 and the V-1 flying bomb with a jet engine . Fascist Italy developed a specialised drone version of the Savoia-Marchetti SM.79 flown by remote control, although the Armistice with Italy was enacted prior to any operational deployment. After World War II development continued in vehicles such as the American JB-4 (using television/radio-command guidance), the Australian GAF Jindivik and Teledyne Ryan Firebee I of 1951, while companies like Beechcraft offered their Model 1001 for

7038-595: The Boeing 747 , had recently made subsonic aircraft significantly more efficient and presented a low-risk option for airlines. While carrying a full load, Concorde achieved 15.8 passenger miles per gallon of fuel, while the Boeing 707 reached 33.3 pm/g, the Boeing 747 46.4 pm/g, and the McDonnell Douglas DC-10 53.6 pm/g. A trend in favour of cheaper airline tickets also caused airlines such as Qantas to question Concorde's market suitability. During

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7176-705: The British Civil Aviation Authority adopted this term, also used in the European Union's Single European Sky (SES) Air Traffic Management (ATM) Research (SESAR Joint Undertaking) roadmap for 2020. This term emphasizes the importance of elements other than the aircraft. It includes elements such as ground control stations, data links and other support equipment. Similar terms are unmanned aircraft vehicle system ( UAVS ) and remotely piloted aircraft system ( RPAS ). Many similar terms are in use. Under new regulations which came into effect 1 June 2019,

7314-510: The Concorde" or " a Concorde". Advertisements for Concorde during the late 1960s placed in publications such as Aviation Week & Space Technology predicted a market for 350 aircraft by 1980. The new consortium intended to produce one long-range and one short-range version, but prospective customers showed no interest in the short-range version, thus it was later dropped. Concorde's costs spiralled during development to more than six times

7452-510: The Garmin G1000 NXi glass cockpit avionics suite. Currently the Archers are used to teach students in obtaining certification as a private pilot and additional training for the instrument rating as well as the more advanced Certified Flight Instructor (CFI) and Certified Flight Instructor - Instrument (CFII) courses. UND Aerospace took delivery of its first Skyhawk, tail number N511ND, in 2008 as

7590-602: The Tupolev Tu-144 . Concorde was the first airliner to have a fly-by-wire flight-control system (in this case, analogue); the avionics system Concorde used was unique because it was the first commercial aircraft to employ hybrid circuits . The principal designer for the project was Pierre Satre, with Sir Archibald Russell as his deputy. Concorde pioneered the following technologies: For high speed and optimisation of flight: For weight-saving and enhanced performance: A symposium titled "Supersonic-Transport Implications"

7728-552: The U.S. Navy in 1955. Nevertheless, they were little more than remote-controlled airplanes until the Vietnam War . In 1959, the U.S. Air Force , concerned about losing pilots over hostile territory, began planning for the use of uncrewed aircraft. Planning intensified after the Soviet Union shot down a U-2 in 1960. Within days, a highly classified UAV program started under the code name of "Red Wagon". The August 1964 clash in

7866-470: The UK CAA on 5 December. Concorde is a tailless aircraft design with a narrow fuselage permitting 4-abreast seating for 92 to 128 passengers, an ogival delta wing and a droop nose for landing visibility. It is powered by four Rolls-Royce/Snecma Olympus 593 turbojets with variable engine intake ramps , and reheat for take-off and acceleration to supersonic speed. Constructed out of aluminium , it

8004-575: The United States Air Force (USAF) employed 7,494 UAVs – almost one in three USAF aircraft. The Central Intelligence Agency also operated UAVs . By 2013 at least 50 countries used UAVs. China, Iran, Israel, Pakistan, Turkey, and others designed and built their own varieties. The use of drones has continued to increase. Due to their wide proliferation, no comprehensive list of UAV systems exists. The development of smart technologies and improved electrical-power systems led to

8142-503: The United States Department of Defense , UAVs are classified into five categories below: Other classifications of UAVs include: There are usually five categories when UAVs are classified by range and endurance: There are usually four categories when UAVs are classified by size, with at least one of the dimensions (length or wingspan) meet the following respective limits: Based on their weight, drones can be classified into 5 categories— . Drones could also be classified based on

8280-456: The hydrogen fuel cell . The energy density of modern Li-Po batteries is far less than gasoline or hydrogen. However electric motors are cheaper, lighter and quieter. Complex multi-engine, multi-propeller installations are under development with the goal of improving aerodynamic and propulsive efficiency. For such complex power installations, battery elimination circuitry (BEC) may be used to centralize power distribution and minimize heating, under

8418-401: The quadcopter design has become popular, though this layout is rarely used for crewed aircraft. Miniaturization means that less-powerful propulsion technologies can be used that are not feasible for crewed aircraft, such as small electric motors and batteries. Control systems for UAVs are often different from crewed craft. For remote human control, a camera and video link almost always replace

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8556-425: The transonic speed range, between Mach 0.95 and 1.7. Kinetic heating from the high speed boundary layer caused the skin to heat up during supersonic flight. Every surface, such as windows and panels, was warm to the touch by the end of the flight. Apart from the engine bay, the hottest part of any supersonic aircraft's structure is the nose , due to aerodynamic heating . Hiduminium R.R. 58, an aluminium alloy,

8694-459: The 1900s, and originally focused on providing practice targets for training military personnel . The earliest attempt at a powered UAV was A. M. Low 's "Aerial Target" in 1916. Low confirmed that Geoffrey de Havilland's monoplane was the one that flew under control on 21 March 1917 using his radio system. Following this successful demonstration in the spring of 1917 Low was transferred to develop aircraft controlled fast motor launches D.C.B.s with

8832-601: The 1973 Yom Kippur war, a few key people from the team that developed this early UAV joined a small startup company that aimed to develop UAVs into a commercial product, eventually purchased by Tadiran and leading to the development of the first Israeli UAV. In 1973, the U.S. military officially confirmed that they had been using UAVs in Southeast Asia (Vietnam). Over 5,000 U.S. airmen had been killed and over 1,000 more were missing or captured . The USAF 100th Strategic Reconnaissance Wing flew about 3,435 UAV missions during

8970-618: The 1980s and 1990s, interest in UAVs grew within the higher echelons of the U.S. military. The U.S. funded the Counterterrorism Center (CTC) within the CIA, which sought to fight terrorism with the aid of modernized drone technology. In the 1990s, the U.S. DoD gave a contract to AAI Corporation along with Israeli company Malat. The U.S. Navy bought the AAI Pioneer UAV that AAI and Malat developed jointly. Many of these UAVs saw service in

9108-594: The 20 aircraft built have been preserved and are on display across Europe and North America. In the early 1950s, Arnold Hall , director of the Royal Aircraft Establishment (RAE), asked Morien Morgan to form a committee to study supersonic transport . The group met in February 1954 and delivered their first report in April 1955. Robert T. Jones ' work at NACA had demonstrated that the drag at supersonic speeds

9246-477: The Americans. Everyone involved agreed that Küchemann's ogee-shaped wing was the right one. The British team was still focused on a 150-passenger design serving transatlantic routes, while France was deliberately avoiding these. Common components could be used in both designs, with the shorter range version using a clipped fuselage and four engines, and the longer one a stretched fuselage and six engines, leaving only

9384-540: The Atlantic Ocean on less than a gallon of fuel" holds this record. Besides the traditional piston engine, the Wankel rotary engine is used by some drones. This type offers high power output for lower weight, with quieter and more vibration-free running. Claims have also been made for improved reliability and greater range. Small drones mostly use lithium-polymer batteries (Li-Po), while some larger vehicles have adopted

9522-462: The Garmin G-1000 equipped Piper Archer and Piper Seminole aircraft. Two Alsim jet training devices are used to provide a basic introduction to turbine engine systems as well as to prepare graduate students for the pace of airline training. In addition, there are various simple instrument panel trainers, a basic instrument simulator computer based instruction (CBI) lab, an FAA Knowledge Test Center, and

9660-460: The M-Wing, for the lower-speed shorter-range category. Both the STAC group and the government were looking for partners to develop the designs. In September 1959, Hawker approached Lockheed , and after the creation of British Aircraft Corporation in 1960, the former Bristol team immediately started talks with Boeing , General Dynamics , Douglas Aircraft , and Sud Aviation . Küchemann and others at

9798-636: The Main Campus. A 260-seat auditorium with full audio-visual and recording capability is located on the second floor. The first floor hosts much of UND Aerospace's computing power as well as UND's 360-degree visual Air Traffic Control Tower simulator. Centered on top of Clifford Hall is UND's Polarimetric Doppler Radar used by the Atmospheric Sciences Department. Ryan Hall is home to UND's air traffic control faculty and UND's 16+ flight simulators, including FAA Level 6 flight training devices for

9936-589: The Middle East, Israeli intelligence tested the first tactical UAVs installed with reconnaissance cameras, which successfully returned photos from across the Suez Canal. This was the first time that tactical UAVs that could be launched and landed on any short runway (unlike the heavier jet-based UAVs) were developed and tested in battle. In the 1973 Yom Kippur War , Israel used UAVs as decoys to spur opposing forces into wasting expensive anti-aircraft missiles. After

10074-542: The RAE continued their work on the slender delta throughout this period, considering three basic shapes; the classic straight-edge delta, the "gothic delta" that was rounded outward to appear like a gothic arch , and the " ogival wing" that was compound-rounded into the shape of an ogee . Each of these planforms had advantages and disadvantages. As they worked with these shapes, a practical concern grew to become so important that it forced selection of one of these designs. Generally

10212-537: The Royal Navy in 1918 intended to attack shipping and port installations and he also assisted Wing Commander Brock in preparations for the Zeebrugge Raid . Other British unmanned developments followed, leading to the fleet of over 400 de Havilland 82 Queen Bee aerial targets that went into service in 1935. Nikola Tesla described a fleet of uncrewed aerial combat vehicles in 1915. These developments also inspired

10350-639: The Standards and Publications Departments, Administrative offices, and a cafeteria. The UND Aerospace Foundation operates a UND Aerospace Foundation Flight Training Center in Phoenix, AZ. The center is located at the Phoenix-Mesa Gateway Airport and the flight school is located on the Chandler-Gilbert Community College campus. UND-Phoenix has an accelerated program where students can become a CFI and get FAA credentials in less than

10488-472: The Syrian air defenses at the start of the 1982 Lebanon War , resulting in no pilots downed. In Israel in 1987, UAVs were first used as proof-of-concept of super-agility, post-stall controlled flight in combat-flight simulations that involved tailless, stealth-technology-based, three-dimensional thrust vectoring flight-control, and jet-steering. With the maturing and miniaturization of applicable technologies in

10626-636: The Tonkin Gulf between naval units of the U.S. and the North Vietnamese Navy initiated America's highly classified UAVs ( Ryan Model 147 , Ryan AQM-91 Firefly , Lockheed D-21 ) into their first combat missions of the Vietnam War . When the Chinese government showed photographs of downed U.S. UAVs via Wide World Photos , the official U.S. response was "no comment". During the War of Attrition (1967–1970) in

10764-456: The UAV industry, is projected to experience a compound annual growth rate of 4.8% over the next decade. This represents a near doubling in market size, from $ 12.5 billion in 2024 to an estimated $ 20 billion by 2034. Crewed and uncrewed aircraft of the same type generally have recognizably similar physical components. The main exceptions are the cockpit and environmental control system or life support systems . Some UAVs carry payloads (such as

10902-518: The US was already involved in a similar project, and that if the UK failed to respond it would be locked out of an airliner market that he believed would be dominated by SST aircraft. In 1959, a study contract was awarded to Hawker Siddeley and Bristol for preliminary designs based on the slender delta, which developed as the HSA.1000 and Bristol 198 . Armstrong Whitworth also responded with an internal design,

11040-517: The United Kingdom signed a treaty establishing the development project on 29 November 1962, as the programme cost was estimated at £70 million (£1.68 billion in 2023). Construction of the six prototypes began in February 1965, and the first flight took off from Toulouse on 2 March 1969. The market was predicted for 350 aircraft, and the manufacturers received up to 100 option orders from many major airlines . On 9 October 1975, it received its French Certificate of Airworthiness , and from

11178-503: The advances of computing technology, beginning with analog controls and evolving into microcontrollers, then system-on-a-chip (SOC) and single-board computers (SBC). Modern system hardware for UAV control is often called the flight controller (FC), flight controller board (FCB) or autopilot. Common UAV-systems control hardware typically incorporate a primary microprocessor, a secondary or failsafe processor, and sensors such as accelerometers, gyroscopes, magnetometers, and barometers into

11316-565: The age of 57. He is buried in Grand Forks , less than a mile away from the UND campus. UND Aerospace maintains facilities including 360 degree air traffic control tower simulators, a remote learning classroom, and a wireless network that is available throughout the entire aerospace complex on the main campus and in any of the buildings at the airport. Funding for additional buildings has already been secured. All School of Aerospace Sciences facilities on

11454-479: The aircraft at Mach 2 without difficulties. During an engine failure the required air intake is virtually zero. So, on Concorde, engine failure was countered by the opening of the auxiliary spill door and the full extension of the ramps, which deflected the air downwards past the engine, gaining lift and minimising drag. Concorde pilots were routinely trained to handle double-engine failure. speeds Concorde used reheat (afterburners) only at take-off and to pass through

11592-405: The aircraft lose thrust on that side but the engine creates drag, causing the aircraft to yaw and bank in the direction of the failed engine. If this had happened to Concorde at supersonic speeds, it theoretically could have caused a catastrophic failure of the airframe. Although computer simulations predicted considerable problems, in practice Concorde could shut down both engines on the same side of

11730-411: The airport's opening. Concorde had initially held a great deal of customer interest, but the project was hit by order cancellations. The Paris Le Bourget air show crash of the competing Soviet Tupolev Tu-144 had shocked potential buyers, and public concern over the environmental issues of supersonic aircraft – the sonic boom , take-off noise and pollution – had produced

11868-400: The arrival of the Cessna 172 Skyhawks, UND's primary fleet consisted of a combination of glass and conventional-gauge Piper Warrior IIIs, which were the primary workhorses of the UND fleet from 1989 to 2010. The last conventional-gauge Warrior was retired in March 2010. On March 28, 2008, UND Aerospace took delivery of a new Cessna Citation Mustang business jet, but sold it in order to purchase

12006-484: The cockpit windows; radio-transmitted digital commands replace physical cockpit controls. Autopilot software is used on both crewed and uncrewed aircraft, with varying feature sets. UAVs can be designed in different configurations than manned aircraft both because there is no need for a cockpit and its windows, and there is no need to optimize for human comfort, although some UAVs are adapted from piloted examples, or are designed for optionally piloted modes. Air safety

12144-665: The construction of the Kettering Bug by Charles Kettering from Dayton, Ohio and the Hewitt-Sperry Automatic Airplane – initially meant as an uncrewed plane that would carry an explosive payload to a predetermined target. Development continued during World War I, when the Dayton-Wright Airplane Company invented a pilotless aerial torpedo that would explode at a preset time. The film star and model-airplane enthusiast Reginald Denny developed

12282-409: The control of a microcontroller unit (MCU). Flapping-wing ornithopters , imitating birds or insects, have been flown as microUAVs . Their inherent stealth recommends them for spy missions. Sub-1g microUAVs inspired by flies, albeit using a power tether, have been able to "land" on vertical surfaces. Other projects mimic the flight of beetles and other insects. UAV computing capability followed

12420-511: The degree of autonomy in their flight operations. ICAO classifies unmanned aircraft as either remotely piloted aircraft or fully autonomous. Some UAVs offer intermediate degrees of autonomy. For example, a vehicle may be remotely piloted in most contexts but have an autonomous return-to-base operation. Some aircraft types may optionally fly manned or as UAVs, which may include manned aircraft transformed into manned or Optionally Piloted UAVs (OPVs). The flight of UAVs may operate under remote control by

12558-553: The development teams met, the French Minister of Public Works and Transport Robert Buron was meeting with the UK Minister of Aviation Peter Thorneycroft , and Thorneycroft told the cabinet that France was much more serious about a partnership than any of the US companies. The various US companies had proved uninterested, likely due to the belief that the government would be funding development and would frown on any partnership with

12696-442: The display hangar where aircraft not in use are sometimes kept. There are 11 heated hangars lining Bravo and Charlie Ramp all owned by UND. These hangars are capable of housing up to 130 aircraft. South of Charlie Ramp is UND's newest hangar, which houses dispatch, flight planning, and general hangar space for the helicopter department . North of Charlie Ramp is UND's Flight Operations Administrative building, which contains offices for

12834-676: The early 2000s, Flight International described Concorde as being "one of aerospace's most ambitious but commercially flawed projects", The consortium received orders (non-binding options) for more than 100 of the long-range version from the major airlines of the day: Pan Am , BOAC , and Air France were the launch customers, with six aircraft each. Other airlines in the order book included Panair do Brasil , Continental Airlines , Japan Airlines , Lufthansa , American Airlines , United Airlines , Air India , Air Canada , Braniff , Singapore Airlines , Iran Air , Olympic Airways , Qantas , CAAC Airlines , Middle East Airlines , and TWA . At

12972-539: The early days of aviation , some being applied to remotely flown target aircraft used for practice firing of a battleship's guns, such as the 1920s Fairey Queen and 1930s de Havilland Queen Bee . Later examples included the Airspeed Queen Wasp and Miles Queen Martinet , before ultimate replacement by the GAF Jindivik . The term remains in common use. In addition to the software, autonomous drones also employ

13110-407: The entire nature of supersonic design. The delta had already been used on aircraft, but these designs used planforms that were not much different from a swept wing of the same span. Weber noted that the lift from the vortex was increased by the length of the wing it had to operate over, which suggested that the effect would be maximised by extending the wing along the fuselage as far as possible. Such

13248-457: The fact that delta wings can produce strong vortices on their upper surfaces at high angles of attack . The vortex will lower the air pressure and cause lift. This had been noticed by Chuck Yeager in the Convair XF-92 , but its qualities had not been fully appreciated. Weber suggested that the effect could be used to improve low speed performance. Küchemann's and Weber's papers changed

13386-584: The first meeting, on 5 November 1956, the decision was made to fund the development of a test-bed aircraft to examine the low-speed performance of the slender delta, a contract that eventually produced the Handley Page HP.115 . This aircraft demonstrated safe control at speeds as low as 69 mph (111 km/h), about one third that of the F-104 Starfighter. STAC stated that an SST would have economic performance similar to existing subsonic types. Lift

13524-469: The first scaled remote piloted vehicle in 1935. Soviet researchers experimented with controlling Tupolev TB-1 bombers remotely in the late 1930s. In 1940, Denny started the Radioplane Company and more models emerged during World War II  – used both to train antiaircraft gunners and to fly attack-missions. Nazi Germany produced and used various UAV aircraft during the war, like

13662-667: The fleet, UND Aerospace's Flying Team practices in 3 Cessna 150's. These aircraft were the original aircraft used for pilot training by Odegard. Aerobatic and spin training is provided in 2 American Champion Super Decathlons . Contract students from Air China fly both of the University's King Air aircraft, the BE-90B. Lastly, the Atmospheric Sciences Department employs a Cessna Citation II for weather and atmospheric research. Students seeking helicopter training train in one of 6 Sikorsky 300C two-seat helicopters. In 2013 UND Aerospace developed

13800-419: The flight deck between the flight engineer 's console and the bulkhead. On some aircraft that conducted a retiring supersonic flight, the flight engineers placed their caps in this expanded gap, wedging the cap when the airframe shrank again. To keep the cabin cool, Concorde used the fuel as a heat sink for the heat from the air conditioning. The same method also cooled the hydraulics. During supersonic flight

13938-582: The fuel needed, "some horribly large aeroplanes" resulted. Based on this, the group considered the concept of an SST infeasible, and instead suggested continued low-level studies into supersonic aerodynamics. Soon after, Johanna Weber and Dietrich Küchemann at the RAE published a series of reports on a new wing planform , known in the UK as the "slender delta". The team, including Eric Maskell whose report "Flow Separation in Three Dimensions" contributed to an understanding of separated flow, worked with

14076-534: The human body, especially hypoxia), as well as other specialized laboratories. The centerpiece of the main floor is the 200-seat Arthur P. Anderson Atmospherium Planetarium and Lecture Bowl. The second floor hosts many of the School's administrative offices and the Regional Weather Information Center. Connected to Odegard Hall by a large, enclosed breezeway is Streibel Hall, which formerly housed UND's Computer Science department. Today, Streibel hall

14214-1007: The intakes which solved the problem. Each engine had its own intake and the nacelles were paired with a splitter plate between them to minimise the chance of one powerplant influencing the other. Only above Mach 1.6 (1,960 km/h; 1,220 mph) was an engine surge likely to affect the adjacent engine. The air intake design for Concorde's engines was especially critical. The intakes had to slow down supersonic inlet air to subsonic speeds with high-pressure recovery to ensure efficient operation at cruising speed while providing low distortion levels (to prevent engine surge) and maintaining high efficiency for all likely ambient temperatures in cruise. They had to provide adequate subsonic performance for diversion cruise and low engine-face distortion at take-off. They also had to provide an alternative path for excess intake of air during engine throttling or shutdowns. The variable intake features required to meet all these requirements consisted of front and rear ramps,

14352-530: The loss rate is high, but we are willing to risk more of them ...they save lives!" During the 1973 Yom Kippur War , Soviet-supplied surface-to-air missile -batteries in Egypt and Syria caused heavy damage to Israeli fighter jets . As a result, Israel developed the IAI Scout as the first UAV with real-time surveillance. The images and radar decoys provided by these UAVs helped Israel to completely neutralize

14490-538: The main UND campus are connected by a series of skyways. Buildings here include Odegard Hall, Clifford Hall, Ryan Hall, and Streibel Hall. In July 2016 a fifth building, Robin Hall opened to accommodate the school's growing research and teaching enterprise in unmanned aerial systems. The complex also includes several other buildings including the Center for Entrepreneurship and the Skalicky Tech Incubator. Odegard Hall

14628-437: The main market, to Washington Dulles from 24 May, and to New York JFK from 17 October 1977. Air France and British Airways remained the sole customers with seven airframes each , for a total production of twenty. Supersonic flight more than halved travel times, but sonic booms over the ground limited it to transoceanic flights only. Its only competitor was the Tupolev Tu-144 , carrying passengers from November 1977 until

14766-413: The metallurgical and fatigue modelling. A test rig was built that repeatedly heated up a full-size section of the wing, and then cooled it, and periodically samples of metal were taken for testing. The airframe was designed for a life of 45,000 flying hours. As the fuselage heated up it expanded by as much as 300 mm (12 in). The most obvious manifestation of this was a gap that opened up on

14904-415: The noise concern, although some of these restrictions were later relaxed. Professor Douglas Ross characterised restrictions placed upon Concorde operations by President Jimmy Carter 's administration as having been an act of protectionism of American aircraft manufacturers. The original programme cost estimate was £70 million in 1962, (£1.68 billion in 2023). After cost overruns and delays

15042-449: The original projections, arriving at a unit cost of £23 million in 1977 (equivalent to £180.49 million in 2023). Its sonic boom made travelling supersonically over land impossible without causing complaints from citizens. World events also dampened Concorde sales prospects; the 1973–74 stock market crash and the 1973 oil crisis had made airlines cautious about aircraft with high fuel consumption, and new wide-body aircraft , such as

15180-446: The podded installation was put forward as simpler with only an inlet cone, however, Dr. Seddon of the RAE favoured a more integrated buried installation. One concern of placing two or more engines behind a single intake was that an intake failure could lead to a double or triple engine failure. While a ducted fan over the turbojet would reduce noise, its larger cross-section also incurred more drag. Acoustics specialists were confident that

15318-717: The presentation, saying that he immediately seized on it as the solution to the SST problem. Brown considers this moment as being the birth of the Concorde project. On 1 October 1956 the Ministry of Supply asked Morgan to form a new study group, the Supersonic Transport Aircraft Committee (STAC) (sometimes referred to as the Supersonic Transport Advisory Committee), to develop a practical SST design and find industry partners to build it. At

15456-471: The programme eventually cost between £1.5 and £2.1 billion in 1976, (£11.4 billion – 16 billion in 2023). This cost was the main reason the production run was much smaller than expected. Concorde is an ogival delta winged aircraft with four Olympus engines based on those employed in the RAF's Avro Vulcan strategic bomber . It has an unusual tailless configuration for a commercial aircraft, as does

15594-483: The project would not be likely to significantly affect other, more important, research efforts. At the time, the UK was pressing for admission to the European Economic Community , and this became the main rationale for moving ahead with the aircraft. The development project was negotiated as an international treaty between the two countries rather than a commercial agreement between companies and included

15732-456: The public and media. Also, the relation of UAVs to remote controlled model aircraft is unclear, UAVs may or may not include remote-controlled model aircraft. Some jurisdictions base their definition on size or weight; however, the US FAA defines any unmanned flying craft as a UAV regardless of size. A similar term is remotely piloted aerial vehicle ( RPAV ). UAVs or RPAVs can also be seen as

15870-522: The public on 7–8 June 1969 at the Paris Air Show . As the flight programme progressed, 001 embarked on a sales and demonstration tour on 4 September 1971, which was also the first transatlantic crossing of Concorde. Concorde 002 followed on 2 June 1972 with a tour of the Middle and Far East. Concorde 002 made the first visit to the United States in 1973, landing at Dallas/Fort Worth Regional Airport to mark

16008-456: The publicity manager at BAC's Filton plant. Reflecting the treaty between the British and French governments that led to Concorde's construction, the name Concorde is from the French word concorde ( IPA: [kɔ̃kɔʁd] ), which has an English equivalent, concord . Both words mean agreement , harmony , or union . The name was changed to Concord by Harold Macmillan in response to

16146-528: The regional SAFECON. Since 1981, when the first complete official competition results of the national SAFECON were recorded, the UND Flying Team has won the NIFA National Championship Trophy a total of 17 times over the course of the last 34 years. Among these 17 championships, the UND Flying Team has recorded a number of multi-year streaks of consecutive championship wins that no other school has been able to match. The first and longest streak

16284-409: The requirement that the powerplant, at Mach 2, tolerate pushovers, sideslips, pull-ups and throttle slamming without surging. Extensive development testing with design changes and changes to intake and engine control laws addressed most of the issues except airfield noise and the interaction between adjacent powerplants at speeds above Mach 1.6 which meant Concorde "had to be certified aerodynamically as

16422-469: The simulations had been correct, and this information was added to pilot training. France had its own SST plans. In the late 1950s, the government requested designs from the government-owned Sud Aviation and Nord Aviation , as well as Dassault . All three returned designs based on Küchemann and Weber's slender delta; Nord suggested a ramjet powered design flying at Mach 3, and the other two were jet-powered Mach 2 designs that were similar to each other. Of

16560-405: The sound barrier in the Concorde (as a passenger) and having flown as a crop-duster to help pay for college, Odegard was no stranger to the varied envelopes of flight. He was quite familiar with the many aspects of aviation and his vision for a well-rounded school that trains pilots in all aspects of flight helped the aviation program at UND become what it is today. Odegard died of cancer in 1998 at

16698-529: The term RPAS has been adopted by the Canadian Government to mean "a set of configurable elements consisting of a remotely piloted aircraft, its control station, the command and control links and any other system elements required during flight operation". UAVs may be classified like any other aircraft , according to design configuration such as weight or engine type, maximum flight altitude, degree of operational autonomy, operational role, etc. According to

16836-448: The three letter company designator as NDU. The company designator, together with a flight/trip number, serves as the aircraft identification for the ATC system in several situations. The company designator and flight/trip number are used instead of the aircraft registration number for ATC security and operational purposes and may be used for the international telecommunications service when its use

16974-540: The three, the Sud Aviation Super-Caravelle won the design contest with a medium-range design deliberately sized to avoid competition with transatlantic US designs they assumed were already on the drawing board. As soon as the design was complete, in April 1960, Pierre Satre , the company's technical director, was sent to Bristol to discuss a partnership. Bristol was surprised to find that the Sud team had designed

17112-903: The time of the first flight, the options list contained 74 options from 16 airlines: The design work was supported by a research programme studying the flight characteristics of low ratio delta wings . A supersonic Fairey Delta 2 was modified to carry the ogee planform, and, renamed as the BAC 221, used for tests of the high-speed flight envelope; the Handley Page HP.115 also provided valuable information on low-speed performance. Construction of two prototypes began in February 1965: 001, built by Aérospatiale at Toulouse, and 002, by BAC at Filton , Bristol. 001 made its first test flight from Toulouse on 2 March 1969, piloted by André Turcat , and first went supersonic on 1 October. The first UK-built Concorde flew from Filton to RAF Fairford on 9 April 1969, piloted by Brian Trubshaw . Both prototypes were presented to

17250-432: The top three performing teams in each of the regional SAFECONs from the prior year receive an invitation to attend the national SAFECON. Similar to a regional SAFECON, the national SAFECON is hosted by a member school that has been selected among the schools that have submitted an application to host. The host school also receives an automatic invitation to participate in the national SAFECON, regardless of their performance in

17388-490: The topic between July and September 1962. The committee rejected the economic arguments, including considerations of supporting the industry made by Thorneycroft. Their report in October stated that it was unlikely there would be any direct positive economic outcome, but that the project should still be considered because everyone else was going supersonic, and they were concerned they would be locked out of future markets. It appeared

17526-450: The war at a cost of about 554 UAVs lost to all causes. In the words of USAF General George S. Brown , Commander, Air Force Systems Command , in 1972, "The only reason we need (UAVs) is that we don't want to needlessly expend the man in the cockpit." Later that year, General John C. Meyer , Commander in Chief, Strategic Air Command , stated, "we let the drone do the high-risk flying ...

17664-522: The wind changing after launch, most of the balloons missed their target, and some drifted back over Austrian lines and the launching ship Vulcano . The Spanish engineer Leonardo Torres Quevedo introduced a radio-based control-system called the Telekino at the Paris Academy of Science in 1903, as a way of testing airships without risking human life. Significant development of drones started in

17802-455: The wing selection. In 1965 the NASA test aircraft successfully tested the wing, and found that it reduced landing speeds noticeably over the standard delta wing. NASA also ran simulations at Ames that showed the aircraft would exhibit a sudden change in pitch when entering ground effect. Ames test pilots later participated in a joint cooperative test with the French and British test pilots and found that

17940-462: The wing to be extensively re-designed. The teams continued to meet in 1961, and by this time it was clear that the two aircraft would be very similar in spite of different ranges and seating arrangements. A single design emerged that differed mainly in fuel load. More powerful Bristol Siddeley Olympus engines, being developed for the TSR-2 , allowed either design to be powered by only four engines. While

18078-464: The wing's centre of pressure (CP, or "lift point") should be close to the aircraft's centre of gravity (CG, or "balance point") to reduce the amount of control force required to pitch the aircraft. As the aircraft layout changes during the design phase, it is common for the CG to move fore or aft. With a normal wing design this can be addressed by moving the wing slightly fore or aft to account for this. With

18216-541: Was already available for development to meet the design requirements. Rolls-Royce proposed developing the RB.169 to power Concorde during its initial design phase, but developing a wholly-new engine for a single aircraft would have been extremely costly, so the existing BSEL Olympus Mk 320 turbojet engine, which was already flying in the BAC TSR-2 supersonic strike bomber prototype, was chosen instead. Boundary layer management in

18354-420: Was an almost unstoppable seven year championship dynasty from 1985 to 1991. Additionally, since 1985 the UND Flying Team has recorded nine second-place finishes, three third-place finishes, and a fourth-place and sixth-place finish in 1993 and 1992 respectively. Prior to the 1986 national SAFECON, only the top performing national team champions were recorded. The placement of the runner-up teams in those prior years

18492-571: Was delivered in November 2016 featuring the new G1000 NXi avionics suite. The current UND Aerospace fleet includes the following aircraft (as of July 2021): Historical UND Aerospace Fleet has included the following aircraft: University of North Dakota aircraft have obtained International Civil Aviation Organization (ICAO) company and telephony designators (call signs) for use in air traffic control (ATC) operations. The U.S. Department of Transportation, Federal Aviation Administration, Order JO7340.2E lists

18630-578: Was hosted by the Royal Aeronautical Society on 8 December 1960. Various views were put forward on the likely type of powerplant for a supersonic transport, such as podded or buried installation and turbojet or ducted-fan engines. Concorde needed to fly long distances to be economically viable; this required high efficiency from the powerplant. Turbofan engines were rejected due to their larger cross-section producing excessive drag (but would be studied for future SSTs). Olympus turbojet technology

18768-675: Was strongly related to the span of the wing. This led to the use of short-span, thin trapezoidal wings such as those seen on the control surfaces of many missiles, or aircraft such as the Lockheed F-104 Starfighter interceptor or the planned Avro 730 strategic bomber that the team studied. The team outlined a baseline configuration that resembled an enlarged Avro 730. This short wingspan produced little lift at low speed, resulting in long take-off runs and high landing speeds. In an SST design, this would have required enormous engine power to lift off from existing runways and, to provide

18906-459: Was the first airliner to have analogue fly-by-wire flight controls. The airliner had transatlantic range while supercruising at twice the speed of sound for 75% of the distance. Delays and cost overruns increased the programme cost to £1.5–2.1 billion in 1976, (£11–16 billion in 2023). Concorde entered service on 21 January 1976 with Air France from Paris-Roissy and British Airways from London Heathrow . Transatlantic flights were

19044-552: Was used throughout the aircraft because it was relatively cheap and easy to work with. The highest temperature it could sustain over the life of the aircraft was 127 °C (261 °F), which limited the top speed to Mach 2.02. Concorde went through two cycles of cooling and heating during a flight, first cooling down as it gained altitude at subsonic speed, then heating up accelerating to cruise speed, finally cooling again when descending and slowing down before heating again in low altitude air before landing. This had to be factored into

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