Gulfstream G200

{{Short description|Business jet}}

{{Infobox aircraft

|name = G200

|image = File:Executive Airlines Gulfstream Aerospace G200 JBM.jpg

|caption = Gulfstream G200

|type = Business jet

|manufacturer = Gulfstream Aerospace

|first_flight = December 25, 1997

|introduction = 1999

|retired =

|status= In service

|produced = 1997–2011

|number_built = 250

|unit cost =

|developed_from = IAI Astra

|variants= Gulfstream G280

}}

The Gulfstream G200, formerly known as the IAI Galaxy, is a twin-engine business jet. It was designed originally by Israel Aerospace Industries (IAI) and was produced by IAI for Gulfstream Aerospace from 1999 through 2011.

Design and development

The G200 was originally named "Astra Galaxy". When Gulfstream Aerospace purchased Galaxy Aerospace in 2001 the model was rebranded as the Gulfstream G200.{{cite web|url=http://airstreamjets.com/gulfstream-g200/|title=Gulfstream G200|publisher=airstreamjets.com|date=2015-11-05|access-date=2017-12-10}} Israel Aircraft Industries' subsidiary Galaxy Aerospace Inc. began designing the Galaxy in the late 1980s in a risk-sharing partnership with the Soviet aircraft design bureau Yakovlev OKB.Gunston, Bill and Yefim Gordon. Yakovlev Aircraft since 1924. London, UK: Putnam Aeronautical Books, 1997. {{ISBN|1-55750-978-6}}. The program officially launched in September 1993. Yakovlev handled design and manufacturing of the forward fuselage and empennage. However, the Russian company had trouble meeting agreed production schedules, and the partnership was ended in 1995.[http://www.flightglobal.com/pdfarchive/view/1996/1996%20-%201456.html "Corporate Aircraft, Astra Jet"]. Flight International, 12–16 June 1996.[http://www.flightglobal.com/articles/1995/10/04/24053/iai-stars-in-galaxy-production-reshuffle.html "IAI stars in Galaxy production reshuffle"]. Flight International, 4 October 1995. This led to another risk-sharing agreement, with EADS Sogerma manufacturing the fuselage and empennage, and IAI being responsible for final assembly and other prime contractor duties.{{cite book |last=Frawley |first=Gerard |title=The International Directory of Civil Aircraft |year=2002 |publisher=Aerospace Publications Pty Ltd |location=Fyshwick ACT, Australia |isbn=1-875671-58-7|page=134}}

File:Cockpit Gulfstream G200.jpg

The Galaxy was based on a new wider fuselage, attached to a strengthened Astra SPX wing with integrated winglets and modified high-lift devices, powered by new 5,700-lb (25.3 kN) thrust Pratt & Whitney Canada PW306 turbofans, and with improved Pro Line 4 avionics and an all-new interior. The decision to use the existing Astra SPX wing imposed a maximum limit on size but allowed a fuselage large enough to accommodate three-abreast seating. The main change from the Astra SPX wing was the introduction of Krueger flaps on the leading edges of the inboard section. These recovered some of the field performance lost as a result of the Galaxy's higher wing loading.{{cite news |url= https://www.flightglobal.com/pdfarchive/view/1998/1998%20-%202761.html?search=IAI%20galaxy |author= Moxon, Julian |title= Exploring the Galaxy |quote= The Galaxy "Super Mid-Size" Business Jet Aims to Lower the Price of Large Cabin Comfort |magazine= Flight International |date= 30 September – 6 October 1998 |pages= 65–69}} It used rubber de-ice boots on wing and horizontal stabilizer leading edges. The aircraft has seating configurations for 8 to 10 passengers. The G200 has a forward-tilting stance when on the ground.

File:Galaxy 4X-IGO FAB Sep1998.jpg

File:Gulfstream Aerospace G200 AN1934122.jpg

The Galaxy first flew on December 25, 1997. By December 1998 it had received certification from the US and Israeli aviation agencies. Deliveries began the following year.[http://www.gulfstream.com/products/g200/ G200 Overview] {{Webarchive|url=https://web.archive.org/web/20110717011219/http://www.gulfstream.com/products/g200/ |date=2011-07-17 }}. Gulfstream. Retrieved May 12, 2009. The Galaxy was renamed "G200" after Gulfstream Aerospace acquired Galaxy Aerospace in June 2001.[http://www.airliners.net/aircraft-data/stats.main?id=226 Israel IAI-1126 Galaxy/Gulfstream G200]. Airliners.net.

File:4X-CVI Rami Mizrahi.jpg

In 2005, Gulfstream began designing a follow-on aircraft. The new model, known as the "G250", was launched in 2008.{{cite news |url= https://www.flightglobal.com/news/articles/nbaa-2008-pictures-gulfstream-launches-g250-set-t-316761/ |title= Gulfstream launches G250 set to dominate super mid-size sector from 2011 |work= Flight Global |date= 5 October 2008 |page= 27}}[http://www.flightglobal.com/articles/2008/10/05/316880/nbaa-2008-gulfstream-know-how-buoys-g250-performance-claims.html "NBAA 2008: Gulfstream know-how buoys G250 performance claims"]. Flight International It was later renamed the Gulfstream G280. The final production G200 rolled off the production line on December 19, 2011; 250 units had been built.{{cite news |title=Last G200 Rolls Off Production Line |url=http://www.aviationtoday.com/the-checklist/75400.html |access-date=December 23, 2011 |newspaper=Aviation Today |date=December 22, 2011 |archive-date=October 21, 2016 |archive-url=https://web.archive.org/web/20161021002924/http://www.aviationtoday.com/the-checklist/75400.html |url-status=dead }}

By 2018, 1999-2007 Gulfstream G200s were priced at $2.395 to $6.25 million.{{cite magazine |url= https://www.ainonline.com/sites/default/files/full-issues/ain_1218.pdf |title= For many models, market hitting the apex |magazine= Aviation International News |author= Mark Huber |date= December 2018 |pages= 20–21, 24 |access-date= 2018-12-27 |archive-date= 2018-12-27 |archive-url= https://web.archive.org/web/20181227181555/https://www.ainonline.com/sites/default/files/full-issues/ain_1218.pdf |url-status= dead }}

Specifications

{{Aircraft specs

|prime units? = kts

|ref=Frawley Gulfstream G200 data[http://www.gulfstream.com/downloads/_downloads/product_spec_sheets/G200%20Specifications.pdf G200 Specifications] {{webarchive|url=https://web.archive.org/web/20141127092224/http://www.gulfstream.com/downloads/_downloads/product_spec_sheets/G200%20Specifications.pdf |date=2014-11-27 }}. Gulfstream. Retrieved May 12, 2009.

|crew=2

|capacity=Typical Seating of 8-10, 18 Max / 4,050 lb (1,840 kg)

|length ft= 62

|length in= 3

|length m= 18.97

|span ft= 58

|span in= 1

|span m= 17.70

|height ft= 21

|height in= 5

|height m= 6.53

|wing area sqft= 369

|wing area sqm= 34.3

|empty weight lb= 19,200

|empty weight kg= 8,709

|max takeoff weight lb= 35,450

|max takeoff weight kg= 16,080

|eng1 name= Pratt & Whitney Canada PW306A

|eng1 type=turbofans

|eng1 number=2

|eng1 lbf= 6,040

|eng1 kn= 26.9

|max speed kts= 487

|max speed mph= 560

|max speed kmh= 900

|max speed note=at altitude

|cruise speed kts= 459

|cruise speed mph= 528

|cruise speed kmh= 850

|cruise speed note= normal cruise at altitude

|range nmi= 3,400

|range miles= 3,910

|range km= 6,300

|range note=at Mach 0.75 with 4 passengers

|ceiling ft= 45,000

|ceiling m= 13,700

}}

See also

References