Editing Gulfstream V (section)

==Specifications==
[[File:Gulfstream V from below (cropped).jpg|thumb|Viewed from below]]
[[File:Gulfstream Aerospace G-V Gulfstream V AN1547227.jpg|thumb|Front view]]

{{Aircraft specs
|ref=[[High-performance Instrumented Airborne Platform for Environmental Research|HIAPER]] GV Brochure<ref>{{cite web |url= https://www.eol.ucar.edu/system/files/brochures/observing_facility/HIAPER/HIAPER_Brochure.pdf |title= Gulfstream GV Brochure |publisher= [[High-performance Instrumented Airborne Platform for Environmental Research|HIAPER]] |access-date= 2016-07-22 |archive-url= https://web.archive.org/web/20160525120956/https://www.eol.ucar.edu/system/files/brochures/observing_facility/HIAPER/HIAPER_Brochure.pdf |archive-date= 2016-05-25 |url-status= live }}</ref>
|prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification,
met(ric) first for all others. You MUST choose a format, or no specifications will show -->

<!-- General characteristics -->
|crew=2
|capacity=15–19<ref name=airliners/>
|length ft=96.4
|span ft=93.45
|height ft=26.85
|wing area sqft=1,137
|wing area note=<ref name=airliners>{{cite web |url= http://www.airliners.net/aircraft-data/gulfstream-aerospace-g-v-gulfstream-v/239 |title= Gulfstream aerospace G-V Gulfstream V |publisher= [[Airliners.net]] |access-date= 2016-07-22 |archive-url= https://web.archive.org/web/20160701010632/http://www.airliners.net/aircraft-data/gulfstream-aerospace-g-v-gulfstream-v/239 |archive-date= 2016-07-01 |url-status= live }}</ref>
|aspect ratio={{#expr:93.45/(1137/93.45)round2}}
|airfoil=
|empty weight lb={{#expr:54500-8300}} <!-- EW = MZFW - PL -->
|empty weight note=, Basic Operating Weight with 4 crew : {{convert|46,800|lbs|kg|0}}<ref name=airliners/>
|max takeoff weight lb=90,500
|more general=
* '''Maximum Landing Weight :''' {{convert|75,300|lbs|kg}}
* '''Maximum Zero Fuel Weight :''' {{convert|54,500|lbs|kg}}
* '''Maximum Fuel Load :''' {{convert|41,300|lbs|kg}}
* '''Maximum Payload :''' {{convert|8,300|lbs|kg}}
* '''Payload w/ Max Fuel :''' {{convert|3,400|lbs|kg}}
* '''Cabin Length :''' {{convert|43.92|feet|m}}
* '''Cabin floor Width :''' {{convert|5.25|feet|m}}
* '''Cabin Height :''' {{convert|6.17|feet|m}}

<!-- Powerplant -->
|eng1 number=2
|eng1 name=[[Rolls-Royce BR710]]A1-10
|eng1 type=turbofan
|eng1 lbf=14,750
|eng1 note=<ref name=typeCert/>

<!-- Performance -->
|max speed mach=0.88
|range nmi= 6500
|range note=,<ref name="2012-05-13PR"/> long range cruise with 4 crew, 8 passengers<ref name=airliners/>
|endurance=14hr 28min<ref name=airliners/>
|ceiling ft= 51,000
|more performance=
* '''Cruise speed :''' {{convert|0.83|Mach|altitude_ft=51000|km/h|0}}
* '''Normal cruise range :''' {{convert|5,500|nmi|km|0}}, with 5 crew, 12 passengers<ref name=C37A/>
* '''Takeoff MTOW, ISA, SL :''' {{convert|6,100|feet|m}}
* '''Climb rate :''' {{convert|4188|ft/min|m/s}}<ref name=airliners/>
* '''Ceiling :''' {{convert|51,000|ft|m}}<ref name=airliners/>
|avionics=
}}