Documents / Official release

Office of the Secretary of Defense: 08_Go_Fast

Department of Defense. Office of the Secretary of Defense. · 2023 · 26 pages · text from the file's own layer

This All-domain Anomaly Resolution Office (AARO) case resolution from the U.S. Department of Defense is dated February 2025. It covers the "Go Fast" FLIR video, which a U.S. Navy F/A-18F recorded off Florida in January 2015. AARO found the object was at about 13,000 feet and moving between 5 and 92 mph once wind is accounted for. It assesses with high confidence that the object showed no anomalous performance and attributes the apparent high speed to motion parallax. A technical appendix explains the calculations.

  • p. 1 …Department of Defense Case: “Go Fast” Case Resolution | February 6, 2025 Case Overview In January 2015…
  • p. 4 …Estimating UAP Location, Speed, and Heading from “Go Fast” FLIR Video Data.08Page determined to be…
  • p. 5 …Estimating UAP Location, Speed, and Heading from “Go Fast” FLIR Video Data February 2025 Introduction In…
  • p. 6 UNCLASSIFIED 6 UNCLASSIFIED Data The only data available to AARO from the “Go Fast” event were…
  • p. 7 …Data extracted from frames at 4239 seconds and 4252 seconds in the “Go Fast” video. UAP…
  • p. 17 …minutes of the time reported with the “Go Fast” event. The windspeed and direction are plotted…
  • p. 18 …for at the approximate location of the “Go Fast” event. Because the exact location and heading…
  • p. 24 …The UAP is going over twice as fast as the wind in somewhat the same direction…
  • p. 26 …the location, speed, and heading of the “Go Fast” UAP was not available at the time…
UNCLASSIFIED
8
UNCLASSIFIED
Figure 4: The three axes defined relative to an air platform in FMV analysis. Longitudinal is the
+x, Transverse is the +y, and Vertical is the +z (pointing down).
This coordinate system was applied to the F/A-18 as depicted in Figure 3. Because the aircraft
altitude was constant over the duration of flight, its path is level and confined to the x-y plane (z
= 0).
Figure 5: The top-down view coordinate system defined with the position of the F/A-18 at the origin with
coordinates [0,0,0]. The aircraft is moving in the +x direction.
With the position of the F/A-18 defined at t1, the location of the UAP relative to this position was
calculated. This calculation was done by defining a line-of-sight (LOS) or “pointing” vector and
then rotating this vector around the axes by the sensor azimuth and elevation angles given in
Table I in order to point to the location of the UAP.
The angle of rotation about the x-axis is the aircraft roll and is denoted by α; the angle of rotation
about the y-axis is the “up and down” motion due to the aircraft pitch or sensor pointing08Page determined to be Unclassified
Reviewed by Chief of Staff, AARO
IAW FY24 NDAA, Section 1841(a)(1)(C)
Date: 2/14/2025

Cases discussed

About this file

Official release, from the nara collection. The PDF is mirrored here; the original link is under it. 26 pages are in the text index: search them above, or from the library's search.