请输入您要查询的百科知识:

 

词条 Sukhoi-Gulfstream S-21
释义

  1. Specifications (S-21)

  2. See also

  3. References

  4. External links

{{Refimprove|date=January 2017}}
name = S-21image = Sukhoi SSBJ project model.jpgcaption =Sukhoi SSBJ project modeldesigner =

}}{{Infobox Aircraft Type

type = Supersonic business jetmanufacturer = Sukhoi Design Bureau/Gulfstream Aerospacefirst flight = introduction = retired = status = primary user = more users = produced = number built =program cost= unit cost = developed from = variants with their own articles =
}}

Sukhoi-Gulfstream S-21 was a projected Russian-American supersonic business jet.

In the early 1990s, Gulfstream Aerospace and the Sukhoi Design Bureau began a joint effort to develop a supersonic small business jet, code named the S-21. Due to questionable market demand for commercial supersonic air travel, commitment to the project weakened and delays mounted.[1]

Gulfstream eventually dissolved the partnership, although Sukhoi continued work on the S-21.

The S-21 would be capable of sustained cruise at Mach 2+ and much research and development has gone into the management of the troublesome transonic effects phenomena associated with near Mach 1 air speeds.

As of 2012, the project had not received any funding for the 2013-2025 development period and appeared to be cancelled.[2]

Specifications (S-21)

{{aircraft specifications|
|jet or prop?=jet
|plane or copter?=plane
|include 'armament' field?=no
|include 'capacity' field?=yes
|switch order of units?=no
|crew=2
|capacity=6–10
|length main=124.2 ft
|length alt=37.86 m
|span main= 65.4 ft
|span alt=19.93 m)
  • Wingsweep: 32° unswept (68° swept

|height main= 27.1 ft
|height alt=8.26 m
|area main=
|area alt=
|empty weight main=54,167 lb
|empty weight alt=24,570 kg
|loaded weight main=
|loaded weight alt=
|useful load main=2,000 lb
|useful load alt=907 kg
|max takeoff weight main=114,200 lb
|max takeoff weight alt=51,800 kg)
  • Fuel: 58,465 lb (26,519 kg

|engine (jet)= Aviadvigatel D-21A1
|type of jet=turbofan
|number of jets=3
|thrust main=16,535 lbf
|thrust alt=73.55 kN
|engine (prop)=
|type of prop=
|number of props=
|power main=
|power alt=
|max speed main=1,483 mph
|max speed alt=2,386 km/h
|cruise speed main=1,483 mph
|cruise speed alt=2,386 km/h
|range main=4,600 mi
|range alt=7,403 km)
  • Range (Mach 1.4): 2,715 mi (4,369 km)
  • Range (Mach 0.95): 4,600 mi (7,403 km

|ceiling main=63,900 ft
|ceiling alt=19,477 m
|climb rate main=
|climb rate alt=
|loading main=
|loading alt=
|thrust/weight=0.43
|power/mass main=
|power/mass alt=
|armament=}}

See also

{{aircontent
|related=
|similar aircraft=
  • Aerion SBJ
  • QSST
  • Quiet Spike
  • Tupolev Tu-444

|lists=
  • List of civil aircraft

|see also=
  • Business jet
  • Hypersonic transport
  • Supersonic business jet
  • Supersonic transport

}}

References

1. ^{{cite web |url=http://www.popularmechanics.com/flight/g2302/11-outlandish-attempts-to-build-the-next-concorde/ |work=Popular Mechanics |accessdate=November 17, 2016 |date=November 24, 2015 |first=Chris |last=Clarke |title=11 Outlandish Attempts To Build The Next Concorde}}
2. ^{{cite web|url=http://www.minpromtorg.gov.ru/reposit/minprom/ministry/fcp/avia2013-2025/GP_aviatciya.pdf|title=Государственная программа Российской Федерации "Развитие авиационной промышленности на 2013 - 2025 годы"|publisher=Минпромторг России|accessdate=2013-03-30|archiveurl=https://www.webcitation.org/6Ftb1D23K?url=http://www.minpromtorg.gov.ru/reposit/minprom/ministry/fcp/avia2013-2025/GP_aviatciya.pdf|archivedate=2013-04-15|deadurl=yes}}

External links

{{commons category-inline|Sukhoi S-21}}{{Sukhoi aircraft}}{{Supersonic transport}}

6 : Abandoned civil aircraft projects|Russian business aircraft 2000–2009|Sukhoi aircraft|Supersonic business jets|Trijets|United States business aircraft 2000–2009

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/9/21 20:30:47