Path: utzoo!censor!geac!torsqnt!jarvis.csri.toronto.edu!utgpu!watserv1!watmath!att!cbnews!military From: ae219dp%prism@gatech.edu (Devon Prichard) Newsgroups: sci.military Subject: Re: Burt Rutan Goes Military Summary: note on fighter speeds Message-ID: <14453@cbnews.ATT.COM> Date: 3 Mar 90 06:08:47 GMT References: <14403@cbnews.ATT.COM> Sender: military@cbnews.ATT.COM Organization: Georgia Institute of Technology Lines: 42 Approved: military@att.att.com From: ae219dp%prism@gatech.edu (Devon Prichard) From: daniel@blake.acs.washington.edu (Daniel Perreault) >Burt Rutan, the man who designed and co-piloted the first non-refueled non-stop >flight around the world has designed and constructed a military jet. ... >It is a fairly small jet with top speed ~500mph. with the current level of capability of SAMs, the typical altitude of a fighter mission may well be below 300 ft AGL. in that case, supersonic flight is rarely possible. the aerodynamic and structural penalties for a supersonic-capable wing are quite high, so by limiting a fighter to subsonic or transonic flight, substantial improvements in range, payload, and low speed manueverability are made possible. most dogfight-type encounters quickly drop down to the 300-400 knot speed (due to the massive increase in drag at high G-levels overcoming the excess thrust of the engine). I imagine most fighter pilots in the dogfight scenario would prefer more Sidewinders and fuel. likewise, for both the attack and interdiction missions, supersonic speed is not necessary. however, due to the time between bomber detection and standoff missile launch, _sustained_ supersonic speed would be very useful for the interception role. I suppose trying to cover all attack/CAS/air defense/interception roles with one aircraft is like trying to use a Corvette on a farm; it gets you to the store fast, but not so good for mowing hay. -- |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||| | Devon Prichard making the world safe for helicopters ... | | ae219dp@prism.gatech.edu | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||