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| Keywords: LiftThrust1.PNG en Graph of corresponding engine lift and thrust forces max of various STOVL aircraft including F-35B V-22 Harrier own TGCP 2010-04-18 <gallery> Image LiftThrust-small1 PNG Without V-22 </gallery> Source is OpenDocument spreadsheet LiftThrust ods at http //www mediafire com/download php zymmzm1xdlj also by this author in public domain please beautify and/or convert to SVG scalable format<br/> Aircraft thrust and lift forces induced by engines not wing lift in a scenario of nearly zero altitude and airspeed <br/> Some aircraft have different thrust in different airspeeds <br/> table is easier to read in edit <br/> Force kN notes <br/> Aircraft Mode Thrust Lift Links to references<br/> F-35B Horizontal 111 0 1 http //www jsf mil/downloads/mediakits/7764 zip<br/> Vertical 0 175 http //www f135engine com/proven-tech/engine_chacter shtml<br/> STOVL 70 105 2 http //www f135engine com/proven-tech/engine_chacter shtml<br/> Afterburner 178 0 1 http //www jsf mil/downloads/mediakits/7764 zip<br/> V-22 Horizontal 253 0 7 http //www flightglobal com/blogs/the-dewline/2009/06/boeing-looks-ahead-to-a-v-23-o html<br/> Vertical 0 230 2; 3 http //www navair navy mil/v22/ fuseaction aircraft main<br/> AV-8B Harrier II<br/> Horizontal 65 0 1; 6 http //www airforce-technology com/projects/harrier/specs html<br/> Vertical 0 86 2; 4 http //www history navy mil/planes/av-8b pdf<br/> F16 Dry thrust 79 0 1 http //www aerospaceweb org/aircraft/fighter/f16/<br/> XV-5 Horizontal 23 0 5 http //www globalsecurity org/military/systems/aircraft/xv-5-specs htm<br/> Vertical 0 71 source unverifyable http //www aero-web org/specs/ryan/xv-5a htm<br/> Notes <br/> 1 Near but not zero airspeed/altitude unfeasible in this position <br/> 2 Thrust is vectorable between 0 and 90 degrees more in most aircrafts Only tail thrust is vectorable in F-35B <br/> 3 Actually higher than this; estimated from max Vertical takeoff weight times gravity constant 23 495kg 9 81m/s 230kN <br/> 4 Normal lift dry 100 RPM for 2 5minutes including splay loss up to 95 86kN available <br/> 5 Unknown variation between horizontal and vertical <br/> 6 Maximum continous Details not available for AV-8B-Plus-version with Pegasus 11-61/Mk 107 at 106kN <br/> 7 Boeing estimates 10 download downwash loss in vertical mode meaning that horizontal thrust is 10 bigger than vertical <br/> TGCP <span class signature-talk >talk</span> 20 30 18 April 2010 UTC Bell-Boeing V-22 Osprey Aircraft comparison diagrams Harrier II aircraft family Lockheed Martin F-35 Lightning II XV-5 Vertifan | ||||
