Skip to main content
. Author manuscript; available in PMC: 2019 Feb 1.
Published in final edited form as: Space Sci Rev. 2017 Dec 13;214(1):19. doi: 10.1007/s11214-017-0439-4

Fig. 8.

Fig. 8

Sample mass measurement configuration. The change in moment of inertia with the TAGSAM arm extended in two positions before and after sampling are measured while the spacecraft rotates about the indicated axis to determine the collected sample mass. No thrusters are used in this configuration, and thus these events are not contributors to hydrazine contamination