NASA-LLIS-1334
Lessons Learned – Cleanliness of Diaphragm Propellant Tanks (2000)
| Organization: | NASA |
| Publication Date: | 21 April 2003 |
| Status: | active |
| Page Count: | 3 |
scope:
Description of Driving Event:
The propellant tanks on the Genesis spacecraft were filled with isopropyl alcohol (IPA) prior to modal and acoustic vibration testing in order to obtain the proper spacecraft dynamic response. IPA was used as a referee fluid in place of the hydrazine propellant because of its similar mass, as well as for safety reasons. When the Genesis tanks were drained about ten days later, levels of particulate and non-volatile residue (NVR) were found that significantly exceeded the cleanliness specification. Both the particulate levels and the NVR were brought back into specification by filling the tank with IPA and draining it several times, followed by vacuum drying.
A cleanliness demonstration test was subsequently performed on
an Atlas Centaur propulsion system hydrazine tank that was of a
design similar to Genesis'. The Atlas tank was also found to be
out-ofspecification with respect to particulate contamination.
After the tank was exposed to the IPA cleaning fluid for about a
day, it was also found to be out-of-specification
The Genesis tank is a titanium sphere with a diaphragm
fabricated from AF-E-332 rubber material. The diaphragm is
incorporated to ensure gas-free propellant expulsion. When empty,
the diaphragm conforms to the lower wall of the tank. As the tank
is filled, the diaphragm reverses toward the upper dome of the
tank. The tank is cleaned at the piece-part level and subjected to
a final cleaning at the assembly level. The ability of cleaning
fluids to remove particulate from the assembled tank during this
final cleaning may have been limited by the fact that the vendor
used only 1 liter of IPA for this procedure. Furthermore, the
vendor has asserted that transportation of a "clean" tank may
result in particulates being released from the faying surfaces near
where the diaphragm is attached to the wall and/or in generation of
particulates due to rubbing of the diaphragm on the tank wall. It
is likely that the out-of-specification
Further materials testing verified that the NVR contamination was a substance leaching out of the rubber diaphragm material following prolonged exposure to IPA. This AF-E-332 diaphragm material has been used in this application since 1974, and contact with hydrazine does not produce degradation of the material or performance problems in propulsion systems. Exposure to IPA for periods of over 4 hours, however, can produce excessive NVR.
Similar tank vendor cleaning processes were used on the Deep Impact project, but it was found that conservative propulsion system filter sizing mitigated the threat of high particulate levels.
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