Luna 15 descent on Jodrell Bank's "Luna 15 and Apollo 11" tape (21 July 1969): extracted data Produced by luna15.py from Luna15-Apollo11.mp3 (https://www.jb.man.ac.uk/multimedia/audio/luna15-apollo11.html, (c) Jodrell Bank Centre for Astrophysics, University of Manchester). The audio itself is not included. All times are seconds into that MP3 (tape time). Audio is resampled to 22050 Hz. carrier.csv the carrier (audio beat note) through the three descent pieces piece 1, 2 or 3 (tape 198.4-232.85, 234.6-252.45, 253.8-277.4 s) t_tape_s centre of the spectrum (0.37 s window, 20 ms steps) f_hz carrier frequency (peak interpolation) snr_db peak over the median of 600-1700 Hz in that spectrum band.csv one row per second: is there more power above the carrier than below it? piece one of the three pieces t_tape centre of the 1 s window above_vs_below_dB mean power 40..300 Hz above the carrier minus 40..300 Hz below it, after dividing every frequency by the receiver noise (piece 3: noise measured after the signal stops, 278.5-305 s; pieces 1-2: each bin's median while the carrier is >350 Hz away). Receiver image lines (k * ~786 Hz - carrier, k = 1..7) are masked within 45 Hz. above_dB_re_noise mean above, dB over that noise below_dB_re_noise mean below, dB over that noise offset_q10/q50/q90 10/50/90 % points of the excess above the carrier (Hz above the carrier) summary.json piece fits (frequency, slope in Hz/s and the line-of-sight acceleration = slope x 0.3249 m at 0/25/50/75/100 % of each piece), the loss of signal (tape time, level, slope at the end, the spoken time check), receiver image-line spacing, the band test (with the image-free part of piece 3 and a carrier-free control), Earth elevation at the published crash sites, closing speed per 100 Hz for flat ground, in-orbit drifts from earlier on the tape, and the hum frequency.