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![]() Ed Rasimus wrote: On 19 Jun 2006 07:50:02 -0700, "Don McIntyre" wrote: While reading through Hans-Heiri Stapfer's "Walk Around MiG-21 Fishbed Part 1" (Squadron-Signal), he makes mention of a temperature probe mounted low on the nose on an MiG-21F-13. Why would a radar rangefinder need to know the OAT? Dunno about MiGs, but every high performance tactical aircraft I ever dealt with had an OAT input to the Central Air Data Computer (or whatever it was called on a particular system.) Air temp is a component of density and that is a factor that impacts range of a weapon. AFAIK temperature determins the speed of sound all on its own. Air density seems to have nothing to do with it unless you get to near space. Air density of course would determin dymanic pressure. Technically the speed of sound is the square root of the ratio of air pressure over air density all multiplied by a constant known as adiatic exponent of air. However as the ratio of pressure to density is a constant at a specific temperature temperature is all that is needed. Best look at it here http://www.sengpielaudio.com/SpeedOfSoundPressure.pdf The WW2 British blind bombing system Oboe made compensations for air density variations so possibly modern radars use it as well, probably not so much for ranging but for doppler or anti-jamming measures. Since dum**** fighter drivers don't like numbers the presentation on the radar screen would be little lines indicating min and max ranges. When the radar gets a range, the computer whiz-bang calculates how far the gizmo can get at the current density altitude. Ed Rasimus Fighter Pilot (USAF-Ret) "When Thunder Rolled" www.thunderchief.org www.thundertales.blogspot.com |
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