Apollo Video Photogrammetry Estimation of Plume Impingement Effects (conference version)

TL;DR

This paper utilizes modern photogrammetry techniques on Apollo lunar landing videos to quantitatively analyze plume impingement effects, including dust ejection angles, particle densities, and large object ejections, informing future lunar landing safety.

Contribution

It introduces a novel application of photogrammetry to Apollo videos for detailed quantitative analysis of lunar plume impingement effects.

Findings

Dust ejection angle estimated at 1-3 degrees

Particle density ranges from 10^8 to 10^13 particles/m^3

Evidence of large object ejection and thrust dependence

Abstract

The Constellation Project's planned return to the moon requires numerous landings at the same site. Since the top few centimeters are loosely packed regolith, plume impingement from the Lander ejects the granular material at high velocities. Much work is needed to understand the physics of plume impingement during landing in order to protect hardware surrounding the landing sites. While mostly qualitative in nature, the Apollo Lunar Module landing videos can provide a wealth of quantitative information using modern photogrammetry techniques. The authors have used the digitized videos to quantify plume impingement effects of the landing exhaust on the lunar surface. The dust ejection angle from the plume is estimated at 1-3 degrees. The lofted particle density is estimated at 10^8 - 10^13 particles/m^3. Additionally, evidence for ejection of large 10-15 cm sized objects and a dependence of ejection angle on thrust are presented. Further work is ongoing to continue quantitative analysis of the landing videos.