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| Re: In Amber Clad loadout discussion | |
| Posted By: Zak Anderson <zakman1989@hotmail.com> | Date: 3/16/05 10:46 p.m. |
In Response To: Re: In Amber Clad loadout discussion (OldNick) : Yes, I was talking about the Yak-141. The main jet nozzle for the F-35B
: "The main engine has a three bearing swivelling exhaust nozzle. The
: The lift fan provides a large proportion of the lift, but the main nozzle
Yes, this i am aware of, but the point i that the lift fan creates a cusion of cool air blowing about which keeps the ground relatively cool. Additionally it means the gass re-ingeted will be relativley cool. : I cited the Yak-141 event mainly because it is the most vivid example I know
66tons of tank, plus 77.5tons of peliacan, being a VTOl the thrut ration needs to be unity or gretaer, so at leasst 140 ton of thrust [assuming no A/G assist]. Yes the downwassh could flip an MBT, look at the horrible V-22, it downwash exceeds that of a hurricane. Now stay away from the pelican, especially you steve loftus, im already working on my pelican physsics article, that tenure is mine, mine i say!!! : These ground-handling problems are not insuperable. The long-serving (since
Also the RCV's draticlly alter airflow, thee are 300 degree Celcius jets going 300km/h. Now the pelican seemss to have the advantage of roof inlets, which helps, additionaly my theory that it uses a replenishing hydrogen jet/rocket [dual cycle] also helps, as it produces a clean reaction, and the excesss water helpss cool the ground underneath it.
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