Thanks to Dean Odle for taking the time and effort to search out and read numerous Documents and bring to light these important proofs, from those who would hide the Glory of God clearly seen through His wonderful Creation.
They took away God’s Firmament and replaced it with Lies.
The father of Lies can no-longer exalt himself above the Most High.
Apocalypse Definition: To UnCover, Reveal, Make Known.
Courtesy of Dean Odle.
Dean’s You Tube Channel.
Dean’s Web Site.
Below here is the three videos above, condensed to 1:45:00
Links to Official Documents used in the First Video
Here’s some of the Military & NASA docs that say “flat earth”
Russia 1948 Shape of the earth unknown.
https://www.nasa.gov/centers/dryden/pdf/88248main_H-1777.pdf
Russian Light Study “Brightness of the firmament” Flat earth :
https://drive.google.com/file/d/1KX7_0tlTAzFEWJ1CWOXQ_K2JnUgbfzb8/view
NASA and military saying it’s flat and motionless Propagation of Electromagnetic Fields Over Flat Earth
http://www.arl.army.mil/arlreports/2001/ARL-TR-2352.pdf
page 9: based upon the signal having a single bounce on a flat Earth
http://www.arl.army.mil/arlreports/2009/ARL-TR-4998.pdf
page 1: Trajectoryof Spinning Projectiles These equations assume a flat Earth.
http://www.arl.army.mil/arlreports/2010/ARL-TR-5118.pdf
page 2: These equations assume a flat Earth
http://www.arl.army.mil/arlreports/2011/ARL-TR-5810.pdf
page 216: “assuming a flat Earth”
http://tycho.usno.navy.mil/ptti/2007papers/paper21.pdf
Page 1: so that a flat-earth approximation provides the best estimate
http://www.arl.army.mil/arlreports/2001/ARL-TN-175.pdf
Page 39: model works over a flat earth
http://www.arl.army.mil/arlreports/2003/ARL-TR-2696.pdf
page 1: transmission loss over flat earth
http://www.arl.army.mil/arlreports/2000/ARL-TR-2156.pdf
page 9: input to a flat earth
http://www.arl.army.mil/arlreports/2003/ARL-MR-563.pdf
page 3: The first is the Earth-fixed coordinate system, which is fixed to the Earth with a flat Earth assumption.
http://www.arl.army.mil/arlreports/2010/ARL-CR-650.pdf
page: 1 flat earth approximation provides the best estimate
http://www.arl.army.mil/arlreports/2002/ARL-TR-2683.pdf
page 32: This model works well over a flat-earth
http://www.arl.army.mil/arlreports/2000/ARL-TR-1812.pdf
page 168: equations of flat-earth trigonometry. (broken link)
http://www.wsmr.army.mil/arlreports/2002/106-17_Telemetry_St…/chapter2.pdf
page 8: The Earth is flat and nonrotating.
http://www.navair.navy.mil/nawcwd/command/counsel/ReadingRoom/NWC_TP5416.pdf
page 2: “In this paper, the rigid body equations of motion over a flat non-rotating earth ”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20070030307.pdf
page 32: “Lastly, the equations of motion for the zeroth-order problem of flight in a vacuum over a flat Earth are presented.”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19940020279.pdf
https://www.nasa.gov/centers/dryden/pdf/88507main_H-2179.pdf
page 14: (2) A flat, nonrotating earth
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19710018599.pdf
page 8: the missile position in space is computed relative to a flat nonrotating earth.
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20040008097.pdf
page:12 “aircraft flying in a stationary atmosphere over flat nonrotating earth”
https://www.nasa.gov/centers/dryden/pdf/88072main_H-1259.pdf
page 108: aircraft flying over flat, nonrotating earth
https://ntrs.nasa.gov/achive/nasa/casi.ntrs.nasa.gov/19890005752.pdf
page 126: “The nonlinear equations of motion used are six-degree-of-freedom equations sith stationary atmosphere and flat, nonrotating earth”
https://ntrs.nasa.gov/achive/nasa/casi.ntrs.nasa.gov/19890007066.pdf
page 2: “The method is limited, however, to application where a flat, nonrotating earth”
https://ntrs.nasa.gov/achive/nasa/casi.ntrs.nasa.gov/19720012071.pdf
page 11: “The nonlinear equations of motion used in this model are general six-degree-of-freedom equations representing the flight dynamics of a rigid aircraft flying in a stationary atmosphere over a flat nonrotating earth”
https://www.nasa.gov/centers/dryden/pdf/88248main_H-1777.pdf
page14: a) The earth is flat and non-rotating.
https://ntrs.nasa.gov/achive/nasa/casi.ntrs.nasa.gov/19790005472.pdf
page 25: The helicopter equations of motion are given in body axes with rerpect to a flat, nonrotating Earth.
https://ntrs.nasa.gov/achive/nasa/casi.ntrs.nasa.gov/19810003557.pdf
page 13: A model frequently used is that of a flat, nonrotating earth.
https://ntrs.nasa.gov/achive/nasa/casi.ntrs.nasa.gov/19650015408.pdf
page 19: These equations assume a rigid vehicle and a flat, nonrotating Earth.
https://www.nasa.gov/centers/dryden/pdf/88733main_H-2465.pdf
page 9: For aircraft problems, the state and measurement models together represent the kinematics of a rigid body for describing motion over a flat, nonrotating Earth
https://ntrs.nasa.gov/achive/nasa/casi.ntrs.nasa.gov/19880014378.pdf
page2: In our minimum time-to-climb problem, the aircraft is modeled as a point mass and the flight trajectory is strictly confined in a vertical plane on a non-rotating, flat earth.
https://ntrs.nasa.gov/achive/nasa/casi.ntrs.nasa.gov/20060053337.pdf
A more comprehensive list can be found here…
FE-Military-Gov-Docs.txt