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{{Redirect|MD-12|the state highway|Maryland Route 12}} {{Redirect|MD-12|Polish aircraft|PZL MD-12|the state highway|Maryland Route 12}}
{{short description|Planned double-deck wide-body airliner, never produced}}
{{Use American English|date=September 2020}}
{{Use dmy dates|date=September 2020}}
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{|{{Infobox aircraft begin {{Infobox aircraft
|name = MD-12 |name= MD-12
|image = Md-12-2.png |image= File:Md-12-2.png
|caption = A computer graphics rendering of the proposed MD-12, a full ] configuration concept |caption= A computer rendering of the proposed MD-12, a full ] configuration concept
|alt=
}}{{Infobox aircraft type
|type = ] ] |type= ] ]
|national origin = ] |national_origin= ]
|manufacturer = ] |manufacturer= ]
|designer = |designer=
|first_flight=
|first flight =
|introduction = |introduction=
|retired = |retired=
|status = Design study, canceled |status= Design study, canceled
|primary_user=
|primary user =
|more users = <!--This field is limited to THREE (3) TOTAL. Please separate with <br/>.--> |more_users= <!--This field is limited to THREE (3) TOTAL. Please separate with <br/>.-->
|produced = |produced=
|number_built=
|number built =
|unit cost = |unit cost=
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}} }}
|}


The '''McDonnell Douglas MD-12''' was an aircraft design study undertaken by the ] company in the 1990s for a "]" aircraft, first conceived as a larger ], then stretched to a 4-engine airliner. It was to be similar in size to the ], but with more passenger capacity. However, the MD-12 received no orders and was canceled. McDonnell Douglas then studied larger ] derivatives named ''MD-XX'' without proceeding. The '''McDonnell Douglas MD-12''' was a large ] concept planned by the ] company in the 1990s. It was first conceived as a ] larger than the ], then stretched to a ] airliner. It was to be similar in size to the ], but with greater passenger capacity through two full-length passenger decks. However, the MD-12 received no orders and was canceled. McDonnell Douglas then studied larger MD-11 derivatives named ''MD-XX'' without proceeding.


==Design and development== ==Design and development==
===Background=== ===Background===
McDonnell Douglas studied improved, stretched versions of the trijet ], named MD-12X<ref name=MDC_brochure> ''md-eleven.net.'' Retrieved: April 14, 2008.</ref> with a possible lower-front passenger deck with panoramic windows.<ref> ''Airliners.net''. Retrieved: October 18, 2007.</ref><ref name=Arthur_p92>Arthur 2002, pp. 92-94.</ref> The MDC board of directors agreed in October 1991 to offer the MD-12X design to airlines. MD-12X had a length of {{convert|237|ft|11|in|m|abbr=on|sigfig=3}} and wingspan of {{convert|212|ft|6|in|m|abbr=on|sigfig=3}}. In November 1991, McDonnell Douglas and Taiwan Aerospace Corporation signed a Memorandum of Understanding to form a company to produce the new design. The new company would have McDonnell Douglas as the majority shareholder (51%) with Taiwan Aerospace (40%) and other Asian companies (9%) having the remaining shares.<ref name=Arthur_p92/> McDonnell Douglas studied improved, stretched versions of the ] trijet, named MD-12X<ref name=MDC_brochure> {{Webarchive|url=https://web.archive.org/web/20080511211119/http://md-eleven.net/MD11-MD12-undeveloped-models |date=2008-05-11}} md-eleven.net. Retrieved: April 14, 2008.</ref> with a possible lower-front passenger deck with panoramic windows.<ref> Airliners.net. Retrieved: October 18, 2007.</ref><ref name=Arthur_p92>{{citation |last=Steffen |first=Arthur |title=McDonnell Douglas MD-11: A Long Beach Swansong |publisher=Hinckley |location=UK: Midland |year=2002 |isbn=1-85780-117-2 |pages=92–94}}</ref> The MDC board of directors agreed in October 1991 to offer the MD-12X design to airlines. The MD-12X had a length of {{convert|237|ft|11|in|m|abbr=on|sigfig=3}} and a wingspan of {{convert |212|ft|6|in|m|abbr=on|sigfig=3}}. In November 1991, McDonnell Douglas and Taiwan Aerospace Corporation signed a Memorandum of Understanding to form a company to produce the new design. The new company would have McDonnell Douglas as the majority shareholder (51%) with Taiwan Aerospace (40%) and other Asian companies (9%) having the remaining shares.<ref name=Arthur_p92/>


===MD-12=== ===MD-12===

In late 1991, McDonnell Douglas made a move to separate its civil and military divisions in a bid to raise the estimated $4 billion development costs needed to develop the MD-12X trijet. Separating the costly military C-17 airlifter development, which had been a drain on the company's resources, from the profit-making production of the MD-80 and MD-11 airliners would make it easier to attract foreign investors for the MD-12X.<ref> ''Flight International,'' November 13–19, 1991.</ref> In late 1991, McDonnell Douglas made a move to separate its civil and military divisions in a bid to raise the estimated $4 billion development costs needed to develop the MD-12X trijet. Separating the costly development of the military ] airlifter, which had been a drain on the company's resources, from the profit-making production of the MD-80 and MD-11 airliners would make it easier to attract foreign investors for the MD-12X.<ref> ''Flight International'', November 13–19, 1991.</ref>


The design grew into the much larger MD-12 with four engines and two passenger decks extending the length of the ]. The length of the main MD-12 variants was {{convert|208|ft|m|abbr=on|sigfig=3}} with a wingspan of {{convert|213|ft|m|abbr=on|sigfig=3}}. The fuselage was {{convert|24|ft|3|in|m|2|abbr=on|sigfig=3}} wide by {{convert|27|ft|11|in|m|abbr=on|sigfig=3}} high.<ref name=Arthur_p92/> The design grew into the much larger MD-12 with four engines and two passenger decks extending the length of the ]. The length of the main MD-12 variants was {{convert|208|ft|m|abbr=on|sigfig=3}} with a wingspan of {{convert|213|ft|m|abbr=on|sigfig=3}}. The fuselage was {{convert|24|ft|3|in|m|2|abbr=on|sigfig=3}} wide by {{convert|27|ft|11|in|m|abbr=on|sigfig=3}} high.<ref name=Arthur_p92/>


McDonnell Douglas unveiled its MD-12 design in April 1992.<ref name=Arthur_p92/> The design was similar in concept to the ] and ], and it would have been larger than the ] with which it would have directly competed. ] had also studied a smaller double-decker design in the 1960s.<ref>Berek, D. ''webshots.com,'' April 4, 2004. Retrieved: July 15, 2011.</ref><ref>Waddington, Terry. ''McDonnell Douglas DC-10''. Miami, Florida: World Transport Press, 2000. ISBN 1-892437-04-X.</ref> McDonnell Douglas unveiled its MD-12 design in April 1992.<ref name=Arthur_p92/> The design was similar in concept to the ] and ], and it would have been larger than the ] with which it would have directly competed. ] also studied a smaller double-decker design in the 1960s for the aircraft that would eventually become the DC-10.<ref>Berek, D. {{Webarchive|url=https://web.archive.org/web/20131227112246/http://rides.webshots.com/photo/1131353000048918155rOFmxM |date=2013-12-27}} webshots.com, April 4, 2004. Retrieved: July 15, 2011.</ref><ref>Waddington, Terry. ''McDonnell Douglas DC-10''. Miami, Florida: World Transport Press, 2000. {{ISBN |1-892437-04-X}}.</ref>


The first flight of the MD-12 was to take place in late 1995, with delivery in 1997.<ref name=Arthur_p92/> Despite aggressive marketing and initial excitement, especially in the aviation press, no orders were placed for the aircraft. MDC lacked the resources after Taiwan Aerospace left the project.<ref name=Arthur_p92/> A new ] widebody has proved to be extremely expensive and complex to develop, even for the remaining aerospace giants Boeing and Airbus, although the massive ], a similar concept to the MD-12, was later brought to fruition.<ref> ''Times Online,'' October 4, 2006.</ref><ref> ''CNN'', March 5, 2007.</ref> The first flight of the MD-12 was to take place in late 1995, with delivery in 1997.<ref name=Arthur_p92/> Despite aggressive marketing and initial excitement, especially in the aviation press, no orders were placed for the aircraft. MDC lacked the resources after Taiwan Aerospace left the project.<ref name=Arthur_p92/> Some skeptics believed that MDC launched the project to lure Boeing into paying a higher price for the company.<ref>{{cite web |last1=Knowlton |first1=Brian |last2=International Herald Tribune |title=Boeing to Buy McDonnell Douglas |url=https://www.nytimes.com/1996/12/16/news/boeing-to-buy-mcdonnell-douglas.html |date= December 16, 1996 |website=New York Times |accessdate= September 25, 2020}}</ref><ref>{{cite web |last1=Bean |first1=Bransom |title=Failure to Launch: The Legacy of the McDonnell Douglas MD-12 Program |url=http://www.avgeekery.com/failure-to-launch-the-legacy-of-the-mcdonnell-douglas-md-12-program/ |website=AV Geekery |date=5 January 2016 |accessdate=23 March 2017}}</ref> A new double-deck widebody has proved to be extremely expensive and complex to develop, even for the remaining aerospace giants Boeing and Airbus, although the massive ], a similar concept to the MD-12, was later brought to fruition,<ref> ''Times Online'', October 4, 2006.</ref><ref>{{citation |url=https://money.cnn.com/magazines/fortune/fortune_archive/2007/03/05/8401277/index.htm |title=Big plane, big problems |first=Nelson D. |last=Schwartz |website=] |date=March 5, 2007}}</ref> but was not a financial success.<ref>{{cite news |last1=Spaeth |first1=Andreas |last2=Rooks |first2=Tim |title=Airbus A380: End of a multibillion-dollar dream |url=https://www.dw.com/en/airbus-a380-the-end-of-a-multibillion-dollar-dream/a-60124995 |access-date=10 October 2023 |agency=] |date=16 December 2021 |language=en}}</ref>


===MD-XX=== ===MD-XX===
With the MD-12 program over, McDonnell Douglas focused on 300 to 400–seat MD-11 derivatives. At the 1996 Farnborough International Air Show, the company presented plans for a new trijet with high-seating and long-range named "MD-XX".<ref> {{webarchive |url=https://web.archive.org/web/20111106191654/http://www.boeing.com/news/releases/mdc/96-221.html |date=2011-11-06}} McDonnell Douglas, September 4, 1996.</ref> The MD-XX was offered in two variants; MD-XX Stretch with a longer fuselage and MD-XX LR for longer range. Both MD-XX variant designs had {{convert|213|ft|m|abbr=on|sigfig=3}} wingspan, the same as MD-12. The MD-XX Stretch was lengthened {{convert|32|ft|m|abbr=on|sigfig=2}} over the MD-11 and had seating for 375 in a typical 3-class arrangement and 515 in all-economy seating. Its range was to be {{convert|7020|nmi|mi km|abbr=on|sigfig=3}}. The MD-XX LR was the same length as the MD-11, had seating for 309 in a typical 3-class arrangement and featured a range of {{convert|8320|nmi|mi km|abbr=on|sigfig=3}}. However, the MDC board of directors decided to end the MD-XX program in October 1996, stating the financial investment for the program was too large for the company.<ref name=Arthur_p92/>
<!-- Deleted image removed: ] -->
With the MD-12 program over, McDonnell Douglas focused on 300 to 400–seat MD-11 derivatives. At the 1996 Farnborough International Air Show, the company presented plans for a new trijet with high-seating and long-range named "MD-XX".<ref> ''McDonnell Douglas,'' September 4, 1996.</ref> The MD-XX was offered in two variants; MD-XX Stretch with a longer fuselage and MD-XX LR for longer range. Both MD-XX variant designs had {{convert|213|ft|m|abbr=on|sigfig=3}} wingspan, the same as MD-12. The MD-XX Stretch was lengthened {{convert|32|ft|m|abbr=on|sigfig=2}} over the MD-11 and had seating for 375 in a typical 3-class arrangement and 515 in all-economy seating. Its range was to be {{convert|7020|nmi|mi km|abbr=on|sigfig=3}}. The MD-XX LR was the same length as the MD-11, had seating for 309 in a typical 3-class arrangement and featured a range of {{convert|8320|nmi|mi km|abbr=on|sigfig=3}}. However, the MDC board of directors decided to end the MD-XX program in October 1996, stating the financial investment for the program was too large for the company.<ref name=Arthur_p92/>


==Variants== ==Variants==
The MD-12 was offered in a few proposed variants.<ref name=Arthur_p92/> The MD-12 was offered in a few proposed variants as listed below.<ref name=Arthur_p92/>


*MD-12 HC (High Capacity) *MD-12 HC (High Capacity)
*MD-12 LR (Long Range) *MD-12 LR (Long Range)
*MD-12 ST (Stretch) *MD-12 ST (Stretch)
*MD-12 Twin (two engine version) *MD-12 Twin (two-engine version)


==Specifications (MD-12 High Capacity design)== ==Specifications (MD-12 High Capacity design)==
] ]


{{Aircraft specs
{{aircraft specifications
|prime units?=kts
<!-- if you do not understand how to use this template, please ask at ] -->
|plane or copter?=plane
|jet or prop?=jet
|ref=McDonnell Douglas promotional materials<ref name=MDC_brochure/> |ref=McDonnell Douglas promotional materials<ref name=MDC_brochure/>
|crew=2 (pilot and co-pilot) |crew=2 (pilot and co-pilot)
|capacity=430 Passengers in 3-class arrangement, up to 511 passengers in high-capacity layout |capacity= Long range: 430 passengers (3-class) / High-capacity: 511 passengers (1-class)
|length main=208 ft 0 in |length ft=208
|length alt=63.40 m |length in=0
|length m=63.40
|span main=213 ft 0 in
|span alt=64.92 m |span ft=213
|span in=0
|height main=74 ft 0 in
|height alt=22.55 m |span m=64.92
|height ft=74
|area main=5,846 ft²
|height in=0
|area alt=543.1
|height m=22.55
|empty weight main=402,700 lb
|wing area sqft=5,846
|empty weight alt=187,650 kg
|wing area sqm=543.1
|loaded weight main=
|loaded weight alt= |empty weight lb=402,700
|max takeoff weight main=949,000 lb |empty weight kg=187,650
|max takeoff weight alt=430,500 kg |max takeoff weight lb=949,000
|max takeoff weight kg=430,500
|engine (jet)=]

|type of jet= high-bypass turbofans
|eng1 name=]
|number of jets=4
|eng1 type= high-bypass turbofans
|thrust main=61,500 lbf
|eng1 number=4
|thrust alt=274 kN
|eng1 lbf=61,500
|thrust original=
|eng1 kn=274
|max speed main=Mach 0.85
|max speed alt= 565 mph, 1,050 km/h |max speed mach=0.85
|max speed more= |max speed kts=565
|cruise speed main= |max speed kmh=1,050
|range nmi=7,170
|cruise speed alt=
|range miles=8,251
|cruise speed more=
|range main=7,170 nmi |range km=13,279
|wing loading lb/sqft=162.3
|range alt=9,200 mi, 14,825 km
|wing loading kg/m2=792.7
|ceiling main=
|ceiling alt=
|climb rate main=
|climb rate alt=
|loading main=162.3 lb/ft²
|loading alt=792.7 kg/m²
|thrust/weight=
}} }}


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* ] * ]
|similar aircraft= |similar aircraft=
* ]-550
* ] * ]
* ] * ] (proposed)
* ] * ]
* ] * ] (proposed)
|lists= |lists=
}} }}
Line 115: Line 108:
;Notes ;Notes
{{Reflist}} {{Reflist}}

;Bibliography
{{Refbegin}}
* Steffen, Arthur. ''McDonnell Douglas MD-11: A Long Beach Swansong''. Hinckley, UK: Midland, 2002. ISBN 1-85780-117-2.
{{Refend}}


==External links== ==External links==
{{Commons category|McDonnell Douglas MD-12}} {{Commons category|McDonnell Douglas MD-12}}
* *
* *



{{Douglas airliners}} {{Douglas airliners}}
{{aviation lists}}


] ]
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] ]
] ]
]

Latest revision as of 09:25, 3 January 2025

"MD-12" redirects here. For Polish aircraft, see PZL MD-12. For the state highway, see Maryland Route 12. Planned double-deck wide-body airliner, never produced

MD-12
A computer rendering of the proposed MD-12, a full double-decker configuration concept
General information
TypeDouble-decker wide-body aircraft
National originUnited States
ManufacturerMcDonnell Douglas
StatusDesign study, canceled

The McDonnell Douglas MD-12 was a large wide-body airliner concept planned by the McDonnell Douglas company in the 1990s. It was first conceived as a trijet larger than the MD-11, then stretched to a quadjet airliner. It was to be similar in size to the Boeing 747, but with greater passenger capacity through two full-length passenger decks. However, the MD-12 received no orders and was canceled. McDonnell Douglas then studied larger MD-11 derivatives named MD-XX without proceeding.

Design and development

Background

McDonnell Douglas studied improved, stretched versions of the MD-11 trijet, named MD-12X with a possible lower-front passenger deck with panoramic windows. The MDC board of directors agreed in October 1991 to offer the MD-12X design to airlines. The MD-12X had a length of 237 ft 11 in (72.5 m) and a wingspan of 212 ft 6 in (64.8 m). In November 1991, McDonnell Douglas and Taiwan Aerospace Corporation signed a Memorandum of Understanding to form a company to produce the new design. The new company would have McDonnell Douglas as the majority shareholder (51%) with Taiwan Aerospace (40%) and other Asian companies (9%) having the remaining shares.

MD-12

In late 1991, McDonnell Douglas made a move to separate its civil and military divisions in a bid to raise the estimated $4 billion development costs needed to develop the MD-12X trijet. Separating the costly development of the military C-17 airlifter, which had been a drain on the company's resources, from the profit-making production of the MD-80 and MD-11 airliners would make it easier to attract foreign investors for the MD-12X.

The design grew into the much larger MD-12 with four engines and two passenger decks extending the length of the fuselage. The length of the main MD-12 variants was 208 ft (63.4 m) with a wingspan of 213 ft (64.9 m). The fuselage was 24 ft 3 in (7.39 m) wide by 27 ft 11 in (8.51 m) high.

McDonnell Douglas unveiled its MD-12 design in April 1992. The design was similar in concept to the Airbus A3XX and Boeing New Large Airplane, and it would have been larger than the Boeing 747 with which it would have directly competed. Douglas Aircraft also studied a smaller double-decker design in the 1960s for the aircraft that would eventually become the DC-10.

The first flight of the MD-12 was to take place in late 1995, with delivery in 1997. Despite aggressive marketing and initial excitement, especially in the aviation press, no orders were placed for the aircraft. MDC lacked the resources after Taiwan Aerospace left the project. Some skeptics believed that MDC launched the project to lure Boeing into paying a higher price for the company. A new double-deck widebody has proved to be extremely expensive and complex to develop, even for the remaining aerospace giants Boeing and Airbus, although the massive Airbus A380, a similar concept to the MD-12, was later brought to fruition, but was not a financial success.

MD-XX

With the MD-12 program over, McDonnell Douglas focused on 300 to 400–seat MD-11 derivatives. At the 1996 Farnborough International Air Show, the company presented plans for a new trijet with high-seating and long-range named "MD-XX". The MD-XX was offered in two variants; MD-XX Stretch with a longer fuselage and MD-XX LR for longer range. Both MD-XX variant designs had 213 ft (64.9 m) wingspan, the same as MD-12. The MD-XX Stretch was lengthened 32 ft (9.8 m) over the MD-11 and had seating for 375 in a typical 3-class arrangement and 515 in all-economy seating. Its range was to be 7,020 nmi (8,080 mi; 13,000 km). The MD-XX LR was the same length as the MD-11, had seating for 309 in a typical 3-class arrangement and featured a range of 8,320 nmi (9,570 mi; 15,400 km). However, the MDC board of directors decided to end the MD-XX program in October 1996, stating the financial investment for the program was too large for the company.

Variants

The MD-12 was offered in a few proposed variants as listed below.

  • MD-12 HC (High Capacity)
  • MD-12 LR (Long Range)
  • MD-12 ST (Stretch)
  • MD-12 Twin (two-engine version)

Specifications (MD-12 High Capacity design)

MD-12 three views

Data from McDonnell Douglas promotional materials

General characteristics

  • Crew: 2 (pilot and co-pilot)
  • Capacity: Long range: 430 passengers (3-class) / High-capacity: 511 passengers (1-class)
  • Length: 208 ft 0 in (63.40 m)
  • Wingspan: 213 ft 0 in (64.92 m)
  • Height: 74 ft 0 in (22.55 m)
  • Wing area: 5,846 sq ft (543.1 m)
  • Empty weight: 402,700 lb (187,650 kg)
  • Max takeoff weight: 949,000 lb (430,500 kg)
  • Powerplant: 4 × General Electric CF6-80C2 high-bypass turbofans, 61,500 lbf (274 kN) thrust each

Performance

  • Maximum speed: 565 kn (650 mph, 1,050 km/h)
  • Maximum speed: Mach 0.85
  • Range: 7,170 nmi (8,251 mi, 13,279 km)
  • Wing loading: 162.3 lb/sq ft (792.7 kg/m)

See also

Related development

Aircraft of comparable role, configuration, and era

References

Notes
  1. ^ "MDC brochures for undeveloped versions of the MD-11 and MD-12." Archived 2008-05-11 at the Wayback Machine md-eleven.net. Retrieved: April 14, 2008.
  2. "MD-11 page." Airliners.net. Retrieved: October 18, 2007.
  3. ^ Steffen, Arthur (2002), McDonnell Douglas MD-11: A Long Beach Swansong, UK: Midland: Hinckley, pp. 92–94, ISBN 1-85780-117-2
  4. "MD-12 divides Douglas." Flight International, November 13–19, 1991.
  5. Berek, D. "Proposed double deck DC-10 design in 1965." Archived 2013-12-27 at the Wayback Machine webshots.com, April 4, 2004. Retrieved: July 15, 2011.
  6. Waddington, Terry. McDonnell Douglas DC-10. Miami, Florida: World Transport Press, 2000. ISBN 1-892437-04-X.
  7. Knowlton, Brian; International Herald Tribune (16 December 1996). "Boeing to Buy McDonnell Douglas". New York Times. Retrieved 25 September 2020.
  8. Bean, Bransom (5 January 2016). "Failure to Launch: The Legacy of the McDonnell Douglas MD-12 Program". AV Geekery. Retrieved 23 March 2017.
  9. "Airbus will lose €4.8bn because of A380 delays." Times Online, October 4, 2006.
  10. Schwartz, Nelson D. (5 March 2007), "Big plane, big problems", CNN
  11. Spaeth, Andreas; Rooks, Tim (16 December 2021). "Airbus A380: End of a multibillion-dollar dream". Deutsche Welle. Retrieved 10 October 2023.
  12. "McDonnell Douglas Unveils New MD-XX Trijet Design." Archived 2011-11-06 at the Wayback Machine McDonnell Douglas, September 4, 1996.

External links

Douglas and McDonnell Douglas airliners
Piston-engined
Jet-engined
Never built
See also: McDonnell 119 / 220
Categories: