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To: Arthur Wildfire! March

“Very confusing and vague.”

I don’t know how a reasonable person could be confused about what I posted. Anyway, at 53 seconds of the video, we can see the wingtip vorticies doing their thing to the contrail. In an earlier thread, I explained that in order for the navigation system in guided missiles to function properly and operate the fin control surfaces correctly, the missile CAN’T be spinning.

http://losangeles.cbslocal.com/2010/11/09/exclusive-raw-video-mysterious-missile-launch-off-california-coast/


327 posted on 12/14/2010 9:19:10 AM PST by Ronald_Magnus
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To: Ronald_Magnus

Just to add, a missile may have small control rockets instead of control fins, but either way, the platform being controlled can’t be spinning.


328 posted on 12/14/2010 9:30:51 AM PST by Ronald_Magnus
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To: Ronald_Magnus

OK, thank you for some meat on the bones there. So if it’s not a missile, is it a special magic jet?


330 posted on 12/14/2010 10:24:48 AM PST by Arthur Wildfire! March (George Washington: [Government] is a dangerous servant and a terrible master.)
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To: Ronald_Magnus

“I don’t know how a reasonable person could be confused about what I posted.” I think most anyone can see for himself how phoney that claim is.


331 posted on 12/14/2010 10:27:08 AM PST by Arthur Wildfire! March (George Washington: [Government] is a dangerous servant and a terrible master.)
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To: Ronald_Magnus; Arthur Wildfire! March
...I explained that in order for the navigation system in guided missiles to function properly and operate the fin control surfaces correctly, the missile CAN’T be spinning.

I posted the following to Ronald_Magnus before. No response then so I guess he had no answer for it.

Title : Stability of Spinning ICBM (Intercontinental Ballistic Missile) in First Stage Boost Phase.

Corporate Author : AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING

Abstract : A computer program is developed to model a spinning intercontinental Ballistic Missile (IICBM) during the first stage boost phase. The equations of motion are derived and presented and a full rotation matrix is used to show the relationship between a launch-centered, nonrotating earth inertial reference frame and the missile body reference frame.

Subject Categories : SURFACE-LAUNCHED GUIDED MISSILES


352 posted on 12/14/2010 6:05:45 PM PST by TigersEye (Who crashed the markets on 9/28/08 and why?)
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