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NASA Scientific and Technical Aerospace Reports

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iefly discussed with respect to impacts on makeup water storage (shipped tanks versus storage in prepackaged food). The<br />

Dual L<strong>and</strong>er Transit Mission was selected for study because it has been considered by the Johnson Space Center Exploration<br />

Office in enough detail to define a reasonable set of scenario options for nominal system operation <strong>and</strong> contingencies. This<br />

study also illustrates the concept that there are multiple, reasonable life support system scenarios for any one particular<br />

mission. Thus, the need for a particular commodity can depend upon many variables in the system. In this study, we examine<br />

the need for makeup water as it depends upon the configuration of the rest of the life support system.<br />

Author<br />

Mars L<strong>and</strong>ing Sites; Mars Missions; Food; Moisture Content; Life Support Systems<br />

20040045264 <strong>NASA</strong> Ames Research Center, Moffett Field, CA, USA<br />

Arc Jet Testing of Carbon Phenolic for Mars Sample Return <strong>and</strong> Future <strong>NASA</strong> Missions<br />

Laub, Bernard; Chen, Yih-Kanq; Skokova, Kristina; Delano, Chad; January 2004; 22 pp.; In English; 55th Pacific Coast<br />

Regional <strong>and</strong> Basic Science Division Fall Meeting, 19-22 Oct. 2003, Oakl<strong>and</strong>, CA, USA; No Copyright; Avail: CASI; A03,<br />

Hardcopy<br />

The objective of the Mars Sample Return (MSR) Mission is to return a sample of MArtian soil to Earth. The Earth Entry<br />

Vehicle (EEV) brings te samples through the atmosphere to the ground.The program aims to: Model aerothermal environment<br />

during EEV flight; On the basis of results, select potential TPS materials for EEV forebody; Fabricate TPS materials; Test the<br />

materials in the arc jet environment representative of predicted flight environment;Evaluate material performance; Compare<br />

results of modeling predictions with test results.<br />

Derived from text<br />

Mars Sample Return Missions; Flight Characteristics; Spacecraft Reentry<br />

20040045269 Jet Propulsion Lab., California Inst. of Tech., Pasadena, CA, USA<br />

Space Weathering: An Ultraviolet Indicator<br />

Hendrix, A. R.; Vilas, F.; [2004]; 2 pp.; In English<br />

Contract(s)/Grant(s): NAG9-1209; No Copyright; Avail: CASI; A01, Hardcopy<br />

We present evidence suggesting that the spectral slope of airless bodies in the UV-visible wavelength range can be used<br />

as an indicator of exposure to space weathering. While space weathering generally produces a reddening of spectra in the<br />

visible-NIR spectral regions, it tends to result in a bluing of the UV-visible portion of the spectrum, <strong>and</strong> may in some cases<br />

produce a spectral reversal. The bluing effect may be detectable with smaller amounts of weathering than are necessary to<br />

detect the longer-wavelength weathering effects.<br />

Author<br />

Space Weathering; Ultraviolet Radiation; Light (Visible Radiation); Lunar Exploration<br />

20040045270 Jet Propulsion Lab., California Inst. of Tech., Pasadena, CA, USA<br />

Vesta’s UV Lightcurve: Hemispheric Variation in Brightness <strong>and</strong> Spectral Reversal<br />

Hendrix, Am<strong>and</strong>a R.; Vilas, Faith; Festou, Michael; Icarus; 2003; ISSN 0019-1035; Volume 162, pp. 1-9; In English<br />

Contract(s)/Grant(s): NAG9-1209; Copyright; Avail: Other Sources<br />

Spectra of asteroid 4 Vesta obtained in October 1990 with the International Ultraviolet Explorer are reanalyzed <strong>and</strong><br />

reinterpreted. A large portion of the eastern hemisphere (based on the prime meridian definition of Thomas et al., 1997a) is<br />

darker at UV Wavelengths than much of the western hemisphere. The UV lightcurve is in contrast with the visible lightcurve,<br />

which shows that the eastern hemisphere is brighter than the western. These IUE spectra of Vesta thus may be evidence for<br />

the ’spectral reversal.‘ first seen on the Moon by Apollo 17. where the visibly brighter lunar highl<strong>and</strong>s are darker than the maria<br />

at far-UV wavelengths. This effect was linked to space weathering when it was noted (Wagner et al., 1987) that the spectral<br />

reversal appears in the laboratory spectra of lunar soils but not powdered lunar rocks. We investigate Vesta’s UV lightcurve<br />

<strong>and</strong> spectral reversal, <strong>and</strong> its possible connection with space weathering. The addition to grain coatings of small amounts of<br />

submicroscopic iron (SMFe) through vapor deposition causes drastic spectral changes at UV-visible wavelengths (Hapke,<br />

2001). while the longer wavelength spectrum remains largely unaffected. Other laboratory results (e.g., Hiroi <strong>and</strong> Pieters,<br />

1998) indicate that the UV-visible wavelength range is affected by simulated weathering processes in a manner similar to what<br />

is seen on Vesta. It is likely that Vesta has experienced relatively minor amounts of space weathering, as indicated by the<br />

spectral reversal, along with the subtle visible-near infrared weathering effects (e.g., Binzel et al., 1997).<br />

Author<br />

Brightness; Eastern Hemisphere; Light Curve; Ultraviolet Spectra; Vesta Asteroid<br />

217

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