Gulfstream V Warning: You are not logged in. Your IP address will be publicly visible if you make any edits. If you log in or create an account, your edits will be attributed to your username, along with other benefits.Anti-spam check. Do not fill this in! ==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=15β19<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= }} Summary: Please note that all contributions to Christianpedia may be edited, altered, or removed by other contributors. If you do not want your writing to be edited mercilessly, then do not submit it here. You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource (see Christianpedia:Copyrights for details). Do not submit copyrighted work without permission! Cancel Editing help (opens in new window) Discuss this page