Follow-On Shaft Seal Evaluation for Future OMS Engine Series Valve Derivations

The objective of this project is to characterize/determine the conditions under which propellant vapor migrates/permeates past the Orbital Maneuvering Subsystem Engine (OMS-E) series valve ball valve pinion shaft seals into the series valve actuators. Initial testing was performed in fiscal year (FY) 2012 and continued in FY 2013. Evidence of nitrogen tetroxide (NTO) and monomethylhydrazine (MMH) propellant vapor leakage across the primary and secondary shafts seals of the four OMS-E series valve ball valve pinions have been found on nearly all OMS engines processed at the NASA White Sands Test Facility since 1996. This leakage results in various forms of internal damage to series valve ball valve pinions and actuator assembly components. Two in-flight anomalies occurred during Shuttle flight history (STS-91 OMS-E serial number [S/N] 107; and STS-101 on OMS-E S/N 111) that were direct results of propellant vapor leakage. Testing was performed in FY 2012 and 2013 to attempt to characterize/determine the conditions under which the vapors migrate/permeate past the redundant (primary and secondary) shafts seals on the ball valve pinions and into the actuator housings. In FY 2012 a "simple soak" test was performed in which NTO and MMH were introduced into their respective cavities in a flight series valve and vapor break-through monitored downstream of the primary and secondary shaft seals of each of the four ball valves using vapor detection devices. The follow-on testing performed in FY 2013 focuses on the MMH part of the series valve. In this test, MMH is introduced into the cavity between the fuel ball valves, the cavity pressurized to 250 pounds per square inch gage (psig), and monitoring performed downstream of the primary and secondary shaft seals using vapor detection devices. FY 2012 soak tests resulted in evidence of NTO vapor permeation past the primary and secondary shaft seals of the oxidizer ball valves in 2.5 and 18.5 hours respectively. While MMH vapor permeation was measured at the primary shaft seal locations of the fuel ball valves in 1.5 hours, no evidence of permeation past the secondary shaft seal was measured after 6 weeks of data logging. This resulted in the follow-on test in FY 2013 to add pressurization of the fuel ball valve cavity to determine if this would result in MMH vapor measurements downstream of the fuel ball valve secondary shaft seal locations. FY 2013 testing will be completed by September 2013 and results compiled in a test report.

This is a mature technology (TRL 9) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.

None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.