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NASA Scientific and Technical Aerospace Reports

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20040073759 Michigan Technological Univ., Houghton, MI<br />

Improving NQR Detection of Materials<br />

Suits, B. H.; Jan. 2001; 6 pp.; In English<br />

Contract(s)/Grant(s): N000173-01-1-G000<br />

Report No.(s): AD-A422685; No Copyright; Avail: CASI; A02, Hardcopy<br />

Recent Collaborative work with the Naval Research Laboratory (NRL) to improve explosive detection using nuclear<br />

quadrupole resonance (NQR) is summarized. The work included aspects of radio-frequency (RF) mitigation particularly<br />

concerning RF coil design for NQR applications in the field, such as l<strong>and</strong> mine detection. Additional studies involving<br />

three-frequency NQR were also pursued.<br />

DTIC<br />

Explosives Detection; Nuclear Quadrupole Resonance<br />

20040074175 Smithsonian Astrophysical Observatory, Cambridge, MA, USA<br />

Feasibility Study of Utilizing Existing Infrared Array Cameras for Daylight Star Tracking on <strong>NASA</strong>’s Ultra Long<br />

Duration Balloon (ULDB) Missions<br />

Tueller, Jack, <strong>Technical</strong> Monitor; Fazio, Giovanni G.; Tolls, Volker; May 2004; 13 pp.; In English<br />

Contract(s)/Grant(s): NAG5-8662; No Copyright; Avail: CASI; A03, Hardcopy<br />

The purpose of this study was to investigate the feasibility of developing a daytime star tracker for ULDB flights using<br />

a commercially available off-the-shelf infrared array camera. This report describes the system used for ground-based tests, the<br />

observations, the test results, <strong>and</strong> gives recommendations for continued development.<br />

Derived from text<br />

Feasibility; Infrared Radiation; Balloon Flight; Daytime; CCD Star Tracker; Long Duration Space Flight<br />

20040074179 <strong>NASA</strong> Goddard Space Flight Center, Greenbelt, MD, USA<br />

Estimation of Aperture Errors with Direct Interferometer-Output Feedback for Spacecraft Formation Control<br />

Lu, Hui-Ling; Cheng, Victor H. L.; Leitner, Jesse A.; Carpenter, Kenneth G.; [2004]; 6 pp.; In English; American Control<br />

Conference 2004, 30 Jun. - 2 Jul. 2004, Boston, MA, USA; No Copyright; Avail: CASI; A02, Hardcopy<br />

Long-baseline space interferometers involving formation flying of multiple spacecraft hold great promise as future space<br />

missions for high-resolution imagery. The major challenge of obtaining high-quality interferometric synthesized images from<br />

long-baseline space interferometers is to control these spacecraft <strong>and</strong> their optics payloads in the specified configuration<br />

accurately. In this paper, we describe our effort toward fine control of long-baseline space interferometers without resorting<br />

to additional sensing equipment. We present an estimation procedure that effectively extracts relative x/y translational exit<br />

pupil aperture deviations from the raw interferometric image with small estimation errors.<br />

Author<br />

Apertures; Error Analysis; Interferometers; Feedback Control<br />

20040074204 Arizona Univ., Tucson, AZ, USA<br />

Acquisition of a High-resolution Inductively Coupled Plasma Mass Spectrometer for Cosmochemical <strong>and</strong> Geochemical<br />

Research<br />

Lauretta, D. S.; [2004]; 3 pp.; In English<br />

Contract(s)/Grant(s): NAG5-11355; No Copyright; Avail: CASI; A01, Hardcopy<br />

The primary goal of our research in this program is to develop new techniques for the analysis of volatile trace elements<br />

in very small samples using inductively coupled plasma mass spectrometry (ICP-MS) in preparation for samples returned by<br />

the Stardust mission. The instrument that will serve as the basis of our experiments is the ELEMENT2 high-resolution<br />

ICP-MS. We have spent the past year designing the laboratory to house this instrument as well as space to store <strong>and</strong> prepare<br />

samples returned by the Stardust mission. Unfortunately, the location that we had initially selected for the instrument turned<br />

out to be insufficient for our needs. This was determined almost eight months into the first year of our funding cycle, after<br />

extensive work including the production of engineering drawings. However, during this time the Lunar <strong>and</strong> Planetary<br />

Laboratory was selected to lead Phoenix, the first Mars Scout mission. As a result of this award LPL purchased a new, 50,000<br />

square foot building. We have acquired 1400 square feet of laboratory space in this new facility. Four-hundred square feet will<br />

be used for a class-100 clean room. This area is designated for storage <strong>and</strong> preparation of extraterrestrial materials. The<br />

additional 1000 square feet will house the ELEMENT2 ICP-MS <strong>and</strong> peripheral devices. This is an enormous amount of space<br />

for this instrument, but it provides plenty of room for expansion in the future. The ICP-MS <strong>and</strong> the clean room facilities have<br />

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