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NASA Scientific and Technical Aerospace Reports

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20060002221 Idaho National Engineering Lab., Idaho Falls, ID, USA, Massachusetts Inst. of Tech., Cambridge, MA, USA,<br />

California Univ., Davis, CA, USA<br />

Predicting Ductile Crack Growth in Engineered Structures<br />

Steffler, E. D.; McClintock, F. A.; Rashid, M. M.; Williamson, R. L.; Lloyd, Q. R.; Jan. 19, 2005; 38 pp.; In English<br />

Report No.(s): DE2005-841394; No Copyright; Avail.: National <strong>Technical</strong> Information Service (NTIS)<br />

The DOE Office of Science-Environmental Management Science Program (EMSP) conducted a High Level Waste<br />

Workshop on January 19 <strong>and</strong> 20, 2005 at the Savannah River Site’s SREL Conference Center. The workshop was organized<br />

to facilitate the exchange of information between university <strong>and</strong> national laboratory scientists <strong>and</strong> contractor <strong>and</strong> DOE<br />

personnel from Idaho, Hanford, <strong>and</strong> Savannah River sites responsible for the management of high level waste. Following<br />

overviews of the Savannah River, Hanford <strong>and</strong> Idaho high level waste programs <strong>and</strong> science <strong>and</strong> technology needs, principal<br />

investigators (PI) for 27 projects reviewed findings <strong>and</strong> progress on their research programs focused on key science <strong>and</strong><br />

technology components of high level waste management. The workshop provided an excellent venue for the PI <strong>and</strong> site<br />

operations personnel to develop contacts <strong>and</strong> facilitate communications which will advance the science <strong>and</strong> technology<br />

resulting from these projects in a manner that will better address the needs of the HLW operations at each of the sites.<br />

NTIS<br />

Crack Propagation; Ductility; Predictions<br />

20060002342 ISRO Satellite Centre, Peenya, Bangalore, India<br />

Lifetime Enhancement of Sputtered MoS2 Film Lubricated Ball Bearings<br />

Rao, A. Anna; Senthil Kumar, S. D. R.; Nagabushanam, S.; Journal of Spacecraft Technology, Volume 15, No. 2; July 2005,<br />

pp. 1-9; In English; See also 20060002338; Copyright; Avail.: Other Sources<br />

Sputtered MoS2 lubrication <strong>and</strong> well-proven ion plated lead lubrication are the basic techniques for applying dry<br />

lubrication. Each process is selected based on the specific application, like definite lifetime, low torque noise <strong>and</strong> speed, Before<br />

selecting the lubricant <strong>and</strong> its process, it is m<strong>and</strong>atory to look into the lifetime endurance history of the lubricant. Based on<br />

individual experience, one can draw analogies for further decisions on the life assessment. We present the literature review<br />

trends in of dry lubricants <strong>and</strong> their attainable endurance life <strong>and</strong> hypothetical estimates of sputtered MoS2 film lubrication<br />

selected with other combinations for long life requirements of ball bearings for spacecraft scanner applications. Finally, we<br />

describe the lifetime achieved with the combination of dry lubricants adapted at STL-ISAC which is 9x10(exp 8) cycles or<br />

greater.<br />

Author<br />

Ball Bearings; Lubricants; Molybdenum Disulfides; Sputtering<br />

20060002381 Marquette Univ., Milwaukee, WI, USA<br />

Role of Distributed Inter-Bristle Friction Force On Brush Seal Hysteresis<br />

Zhao, Helen; Stango, Robert; 2004 <strong>NASA</strong> Seal/Secondary Air System Workshop, Volume 1; October 2005, pp. 209-222; In<br />

English; See also 20060002371; Original contains color illustrations; No Copyright; Avail.: CASI: A03, Hardcopy<br />

The micro-moment can give rise to a delayed filament displacement as the shaft undergoes transient excursion <strong>and</strong> moves<br />

radially toward bristle pack ( uploading). However, as the shaft returns back to its concentric position ( downloading), the<br />

filament CANNOT completely recover from its deformed position <strong>and</strong> remains locked in an alternate configuration.<br />

Consequently, an annular gap is generated between the fiber tips <strong>and</strong> shaft surface, which promotes brush seal leakage <strong>and</strong><br />

reduces turbomachinery performance.In general, for a given brush seal, the annular gap increases linearly as the micro moment<br />

m* is increased. The brush seal having a shallowest lay angle (15deg) results in the smallest annular gap, indicating that a<br />

brush seal design with shallow lay angle is least prone to hysteresis phenomenon, <strong>and</strong> can lead to improved performance.<br />

Derived from text<br />

Brush Seals; Leakage; Shafts (Machine Elements); Turbomachinery; Friction; Deformation<br />

20060002405 Department of Energy, Las Vegas, NV, USA<br />

Dry Transfer Facility Criticality Safety Calculations<br />

S<strong>and</strong>ers, C. E.; May 2005; 84 pp.; In English<br />

Report No.(s): DE2005-841275; No Copyright; Avail.: National <strong>Technical</strong> Information Service (NTIS)<br />

This design calculation updates the previous criticality evaluation for the fuel h<strong>and</strong>ling, transfer, <strong>and</strong> staging operations<br />

to be performed in the Dry Transfer Facility (DTF) including the remediation area. The purpose of the calculation is to<br />

91

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