For anyone else curious, it's from the hydrazine tank's rubber diaphragm. Tubes inside the thrusters, which direct fuel to the catalyst beds, had openings taken from 250 um diameter down to 35 um.[1]
The 28" spherical tank[2] has a rubber hemisphere to separate hydrazine from pressurant (He? N?). The diaphragm is EDPM that's teflon and silica filled.[3] The silica particles are for (tensile?) strengthening. It has a leaching issue (discussed in [2] page17).
PSI was a small SoCal company. Derivative tank used for Shuttle APU. Same material used since 1975.
For anyone else curious, it's from the hydrazine tank's rubber diaphragm. Tubes inside the thrusters, which direct fuel to the catalyst beds, had openings taken from 250 um diameter down to 35 um.[1]
The 28" spherical tank[2] has a rubber hemisphere to separate hydrazine from pressurant (He? N?). The diaphragm is EDPM that's teflon and silica filled.[3] The silica particles are for (tensile?) strengthening. It has a leaching issue (discussed in [2] page17).
PSI was a small SoCal company. Derivative tank used for Shuttle APU. Same material used since 1975.
[1] a story https://www.jpl.nasa.gov/news/voyager-1-team-accomplishes-tr... [2] nice paper https://scholar.google.com/scholar?q=review+and+history+of+p... [3] meh, color pic Low cost derivative tanks... https://scholar.google.com/scholar?q=AIAA+99-2831