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#1
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![]() "karl gruber" wrote in message ... I've been searching "Google" to find information on jet takeoff and landing performance. I've searched AOPA and NBA, but can't find what I want. I'm looking for a good dissertation on V1, V2, VR, BFL, second segment climb, etc. V1 is the take off decision speed. If you lose an engine below this speed, you shutdown and stop on the runway. If you lose it after you attain this speed, you continue on the remaining engine(s). Vr is the rotate speed, where you normally would lift the nose on takeoff. V2 is the takeoff safetly speed, the (initial) climbout speed if you've lost an engine. It varies from there depending on the aicraft, after reaching a given speed (usually something like V2+10 knots or something), there are procedures for raising flaps, etc... and new speeds to go with them. |
#2
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"Ron Natalie" writes:
"karl gruber" wrote in message ... I've been searching "Google" to find information on jet takeoff and landing performance. I've searched AOPA and NBA, but can't find what I want. I'm looking for a good dissertation on V1, V2, VR, BFL, second segment climb, etc. V1 is the take off decision speed. If you lose an engine below this speed, you shutdown and stop on the runway. If you lose it after you attain this speed, you continue on the remaining engine(s). Vr is the rotate speed, where you normally would lift the nose on takeoff. V2 is the takeoff safetly speed, the (initial) climbout speed if you've lost an engine. It varies from there depending on the aicraft, after reaching a given speed (usually something like V2+10 knots or something), there are procedures for raising flaps, etc... and new speeds to go with them. And at least for the 'heavies' I understand these values depend on the actual loading and density altitude conditions, rather than being fixed constants. -- David Dyer-Bennet, , www.dd-b.net/dd-b/ RKBA: noguns-nomoney.com www.dd-b.net/carry/ Photos: dd-b.lighthunters.net Snapshots: www.dd-b.net/dd-b/SnapshotAlbum/ Dragaera/Steven Brust: dragaera.info/ |
#3
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On 2003-11-20 15:34:21 -0800, David Dyer-Bennet said
And at least for the 'heavies' I understand these values depend on th actual loading and density altitude conditions, rather than bein fixed constants You don't even have to be that heavy For a Lear 35, the takeoff weight tabular charts show weights between 10,000 and 18,300 and the speeds vary in a range of about 103-141 for V1, 125 to 143 for VR, and 124 to 146 for V2. Note that V1 is the only speed that depends on density altitude. The others vary onl with weight -- Larry Fransso Seattle, W (This post has been manually formatted for your reading pleasure.) |
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