A CMBR Measurement Reproduced A Statistical Comparison of MSAM1-94 to MSAM1-92
DECHEN

REV. DE CIÊNCIA & TECNOLOGIA, Piracicaba, v. 11, n. 21, p. 1-73, jan./jun. 2003.R EVISTA DE C IÊNCIA& T ECNOLOGIA • 211COMISSÃO EDITORIALN IVALDO L EMOS C OPPINI – presidente (Engenharia de Produção) K LAUS S CHÜTZER (Engenharia Mecânica)N ELSON C ARVALHO M AESTRELLI (Gestão da Produção)N IVALDI C ALONEGO JÚNIOR (Ciência da Computação)SÔNIA M ARIA M ALMONGE (Engenharia Química)COMITÊ CIENTÍFICOB ERT L AUWERS (Katholieke Universiteit Leuven –Bélgica)C ARLOS A LBERTO G ASPARETTO (Facens/Unicamp –ESTEVAL project partners.– Feature Based Integrated Design Environment.Identification of interdependencies between manufacturing features.Unsuitable finishing quality (Schützer et al., 1999).After considering several possibilities, which could result in this poor surface quality cutting tool geometry , clamping and balancing of the tool system, technological parameters and machining set-ups, it was realized, that the problem came from the CNC of the machine tool, which was incapable of processing the NC program as fast as the feed rate defined in the NC program. So the machine reaches the point refereed in one line of the program and the information to move the tool to the next point was not processed yet, then the machine had to wait a couple of milliseconds to start moving again.This incompatibility between the feed rate defined in the NC program and the processing time of the CNC results in two different situations according to the CNC used:poor surface quality – the CNC tries to move the machine at the programmed feed rate, but it can-Improper surface finishingThe workpiece used and the finishing tool path.The roughing and semi-finishing operations were accomplished using exactly the same technological parameters and cutting strategies for all workpieces.The comparison analysis was done only during the finishing operation and the same technological para-meters, cutting strategies and tools were used in both cases. The finishing operation was distinguished by the methodology of interpolation. The trajectory of the finishing tool path is shown in figure 3. For this operation it was used a 10 mm ball end mill tool at 10000 rpm and the programmed feed rate was 2000 mm/min.YSISThe results of the machining experiments considering the NC program size, the time required to exe-cute the program and the surface quality in terms of roughness and superficial texture were compared and the conclusions are presented below.NC Program SizesThe table 2 presents the finishing programs sizes calculated for both methods. It proves that less infor-mation are required to describe tool paths by the circular/linear method, thus reducing the program size byMETHOD P ROGRAM SIZE N UMBER586 kbCircular/linear83 kb• V. 11, Nº 21 – pp. 29-36Regions where the feed rate as reduced.2000 mm/min660 mm/min 1500 mm/min700 mm/min2000 mm/minRoughness AnalysisIt was used a digital Surftest Equipment to obtain the Ra and Rz parameters. It was analyzed the same areas for all workpieces. Practically, there are not differences between the roughness parameters for both interpolation methods.Surface T exture AnalysisIt was possible to visually verify the differences between the surfaces of both methods. The circular/ linear workpieces are smoother than the linear ones. The figure 5 shows this texture.Irregular surface texture Regular surface textureBesides those transversal marks at the workpiece machined by the linear interpolation, this method also gives a deficient quality in the longitudinal direction, as it is seen in the next photos taken by a CCD camera connected in an microscopy.Figure 6 was taken using a microscopy with magnification 10x of the linear part. The vertical marks are the cusp heights left by the ball end mill tool. The steps-over of the tool path is on the horizontal direc-Fig. 6. Uneven cusps from a linear workpiece.Fig. 7. Even cusps from a circular/linear workpieceIn linear interpolation method is possible to see uneven cusp heights, what can difficult drastically the hand finishing afterwards. This problem is not seen at the workpieces milled by the circular/linear method, as shown in figure 7. It happens due to the more constant cutting movements.In this method, the cusps height are much more uniform, what can help the manual finishing afterwards, by decreasing this process time, and improving the accuracyCONCLUSIONThe High Speed Cutting T echnology can be attractively applied in die and mould manufacturing, among others applications. However, there are several other technologies in the process chain that must be considered to support an efficient HSC process.R EVISTA DE C IÊNCIA & T ECNOLOGIA • V. 11, Nº 21 – pp. 29-36。
离子色谱测定唾液葡萄糖含量方法的建立及评估

•论著•离子色谱测定唾液葡萄糖含量方法的建立及评估徐春I窦倩2汪诗文2章子锋?戴庆2'解放军总医院第三医学中心内分泌科,北京1()()()39;2国家纳米科学中心,中国科学院卓越中心,中国科学院纳米光子材料与器件重点实验室,北京10()190徐春和窦倩对本文有同等贡献通信作者:戴庆,Email:***************,电话:************【摘要】目的建立用离子色谱测定唾液中葡萄糖浓度的方法。
方法利用热变性法去除唾液中的蛋白质,以CarboPac PA20(3x30mm)作为保护柱.CarboPac PA20(3xl50mm)作为分析柱进行离子色谱分析。
以超纯水(A),250mmol/L NaOH溶液(B),500mmol/L NaAc(C)为淋洗液进行梯度洗脱,采用脉冲安培检测器检测”结果本方法在0.04-0.12mgn.范围内具有较好的线性关系,线性相关系数^.9967:葡萄糖的检出限是0.002mg/L;重复性测量相对标准偏差(RSD)的平均值为0.75%,加标冋收率平均值为103.07%0结论本方法操作简便、灵敏度高、准确性好、结果稳定,可用于唾液中葡萄糖含量的测定。
【关键词】离子色谱;唾液;筍萄糖;糖尿病;无创检测基金项目:中国科学院科技服务网络计划(STS计划)(K町-STS-ZDTP-063);国家重点研发计划(2016YFA0201600)DOI:10.3760/.l15807-20200623-00194Establishment,evaluation,and determination of saliva glucose concentration by ion chromatography XuChun1,Dou Qian2,Wang Shiwen2,Zhang Zifeng2,Dai Qing2'Department of Endocrinology,3rd Medical Center,PLA General Hospital,Beijing100039,China;2CAS Key Laboratory of Nanophotonic Materials(uid Devices,CAS Center for Excellence in Na/ioscience,National Center forNanoscience and Technology,Beijing100190,ChinaXu Chun and Dou Qian contributed equally to this articleCorresponding author:Dili Qing,Email:***************,Tel:************[Abstract]Objective To establish an analytical method for measuring the concentration of glucose insaliva by ion chromatography.Methods The proteins in saliva were removed by thermal denaturation method,CarboPac PA20(3x30mm)was used as a protective column and CarboPac PA20(3x150mm)was used as ananalytical column for ion chromatography analysis.Gradient elution was carried out with A:ultra-pure water,B:250mmol/L NaOH solution and C:500tnmol/L NaAc solution.Pulsed ampere detector was used for detection.Results This method had a good linear relationship in the range of0.04to0.12mg/L,with a linear relation coefficient of0.9967.The detection limit of glucose was2|xg/L,the mean value of the relative standard deviation(RSD)of the repeatability measurement was0.75%,and the average spike recovery was103.07%.Conclusion Thismethod is simple,sensitive,accurate and stable,and can be used for the detennination of glucose concentration insaliva.[Key words]Ion chromatography;Saliva;Glucose;Diabetes;Non-invasive detectionFund program:Science and Technology Service Network Plan of Chinese Academy of Sciences(STS Plan)(KFJ-STS-ZDTP-063);National Key Research and Development Plan(2016YFA0201600)DOI:10.3760/.l15807-20200623-00194唾液由唾液腺(腮腺、颌下腺、舌下腺、小涎腺)分泌,在口腔内起帮助消化、湿润和保护黏膜的作用。
BSEN13697-2015Chemicaldisinfectantsandantiseptics.Quantitativenon-poroussurfacetestforthe

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a selection of measurement results -回复

a selection of measurement results -回复选定主题:[一组测量结果]第一步:引言(100-150字)本文将深入探讨一组测量结果,并逐步回答与其相关的问题。
我们将以科学准确性为基础,以合理推理和相关证据为支撑,共同探究这些测量结果的意义和可能的解释。
第二步:概述测量结果(150-200字)首先,让我们简要介绍这组测量结果。
这些结果涉及多个领域,包括物理学、生物学和经济学等。
我们收集了各种实验和调查数据,这些数据对于我们理解和解决当前问题至关重要。
本文将对其中一些测量结果进行详细分析和解释,以便更好地理解它们的含义。
第三步:重要测量结果的详细分析(800-1000字)接下来,我们将深入分析一些关键的测量结果,以便更好地理解它们。
我们将选择几个代表性的结果,涵盖不同领域,以获得更全面的认识。
首先,让我们考虑一项物理学实验的结果。
该实验旨在测量重力加速度,以确定地球表面的重力场强度。
通过精确地测量时间和物体的自由落体运动,我们得出了一个平均值,并计算了其误差范围。
这些结果对于我们理解地球的物理特性和基本常数非常重要,以及对于未来的科学研究和技术应用有着深远的影响。
接着,我们转向生物学领域的一个测量结果。
通过对一群人进行健康调查和评估,我们得出了一个关于肥胖率的统计数据。
这些数据显示了不同年龄组和性别之间的肥胖率差异,并提供了对这一全球问题的见解。
通过这些结果,我们可以加深对肥胖症的根源和其潜在健康影响的理解,并为制定预防措施和干预政策提供依据。
最后,让我们来看一个经济学领域的测量结果。
通过对某个国家的经济指标进行调查和收集,我们得到了一组有关就业率、通货膨胀率和经济增长率的数据。
这些结果对于政策制定者和经济学家来说至关重要,因为它们可以揭示经济的整体健康状况和趋势,进而帮助他们制定适当的政策和措施来促进经济发展。
通过这些详细分析,我们可以更好地理解这组测量结果的重要性和意义。
Apparatus and method for determining the amount of

专利名称:Apparatus and method for determining the amount of entrapped gas in a material发明人:Charles E. Lee,John D. Della-Santina申请号:US09/132630申请日:19980811公开号:US06082174A公开日:20000704专利内容由知识产权出版社提供摘要:An entrapped gas measuring apparatus includes a reservoir housing with a reservoir which is adapted to receive a material sample and to expand according to an expansion of the material sample when a negative pressure is applied externally to the reservoir. A parameter indicating the change in volume of the reservoir during the expansion, such as the actual change of volume of the reservoir or a change in position of a moveable wall which at least in part defines the reservoir, is detected by a detector. A processor coupled to the detector is used to determine the amount of entrapped gas based upon the detected parameter. The amount of entrapped gas determined by the processor may be the percent volume of the entrapped gas in relation to the overall volume of the sample, or may be the actual volume of the entrapped gas in the sample. Based at least in-part upon the measured amount of entrapped gas within the sample, the processor is further adapted to determine at least one of: percent volume of the substrate in the sample in relation to the overall volume of the sample; actual volume of the substrate in the sample; or density of the sample or substrate within the sample. The entrapped gas measuring apparatus may be used to produce a material having a known amount of entrapped gas by: making a first material according to a first method andwhich has a first amount of entrapped gas; applying a negative pressure to the sample such that the sample expands from a first volume to a second volume; detecting a parameter which is indicative of the change of sample volume under the applied negative pressure; comparing the detected parameter with a predetermined range for the parameter; and, if the detected parameter is not within the predetermined range, making a second material according to a second method which has a second amount of entrapped gas that is within the predetermined range.申请人:BENCHTOP MACHINE AND INSTRUMENT, INC.代理人:James C. Peacock III,John P. O'Banion更多信息请下载全文后查看。
fluorescence quantitative analysis -回复

fluorescence quantitative analysis -回复"Fluorescence quantitative analysis" refers to a technique used to measure the concentration of a substance by examining its fluorescence properties. This technique is commonly employed in various scientific fields such as chemistry, biology, and environmental science. In this article, we will explore the principles behind fluorescence quantitative analysis, the instruments used, and some applications of this technique.1. Introduction to Fluorescence:Fluorescence is a phenomenon exhibited by certain substances when they absorb light at a specific wavelength and emit light at a longer wavelength. This emission of light is called fluorescence. It occurs due to the excitation of electrons in the atoms or molecules of the substance.2. Principles of Fluorescence Quantitative Analysis: Fluorescence quantitative analysis is based on the principle that the intensity of fluorescence emitted by a substance is directly proportional to its concentration. This principle forms the basis for detecting and measuring the concentration of various substances.3. Instrumentation for Fluorescence Quantitative Analysis:a. Fluorometers: Fluorometers are the primary instruments used for fluorescence quantitative analysis. They consist of a light source, filters to select the excitation and emission wavelengths, and a detector to measure the emitted light.b. Fluorescence Microscopes: Fluorescence microscopes combine traditional microscopy with fluorescence detection. They allow for the visualization and quantification of fluorescently labeled samples.c. Flow Cytometers: Flow cytometers employ fluorescence to analyze individual cells or particles in a solution. They can measure multiple parameters simultaneously, providing detailed information about the sample.4. Process of Fluorescence Quantitative Analysis:a. Selection of fluorophore: The first step involves choosing a suitable fluorophore that exhibits fluorescence properties when bound to the target substance.b. Calibration Curve: A calibration curve is constructed by measuring the fluorescence intensity at different known concentrations of the target substance. This curve establishes therelationship between fluorescence intensity and concentration. c. Sample Preparation: The sample is prepared by incorporating the fluorophore into the solution containing the substance to be quantified.d. Excitation and Emission: The sample is excited with a specific wavelength of light, and the emitted fluorescence is detected and measured.e. Comparison with Calibration Curve: The fluorescence intensity of the sample is compared with the calibration curve to determine its concentration.5. Applications of Fluorescence Quantitative Analysis:a. Biochemical Assays: Fluorescence quantitative analysis is widely used in biochemical assays to determine the concentration of biomolecules such as DNA, proteins, and enzymes.b. Drug Discovery: Researchers use fluorescence quantitative analysis to screen potential drug candidates and study their interactions with target molecules.c. Environmental Monitoring: This technique is utilized to measure the concentration of pollutants in water and air, facilitating environmental monitoring and assessment.d. Medical Research: Fluorescence quantitative analysis helpsdiagnose diseases and monitor their progression by quantifying specific biomarkers in biological samples.In conclusion, fluorescence quantitative analysis is a versatile technique that enables precise and sensitive measurements of substance concentrations. It finds extensive applications in various scientific fields and continues to contribute to advancements in research and analysis.。
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a rXiv:as tr o-ph/96317v15Mar1996Submitted to Ap.J.Letters ;astro-ph/9603017A CMBR Measurement Reproduced:A Statistical Comparison of MSAM1-94to MSAM1-92C.A.Inman 1,E.S.Cheng 2,D.A.Cottingham 3,D.J.Fixsen 4,M.S.Kowitt 2,S.S.Meyer 1,L.A.Page 5,J.L.Puchalla 2,J.E.Ruhl 6,and R.F.Silverberg 2ABSTRACT The goal of the second flight of the Medium Scale Anisotropy Measurement (MSAM1-94)was to confirm the measurement of cosmic microwave background radiation (CMBR)anisotropy made in the first flight (MSAM1-92).The CMBR anisotropy and interstellar dust emission signals from the two flights are compared by forming the sum and difference of those portions of the data with the same pointings on the sky.The difference data are consistent with a null detection,while the summed data show significant signal.We conclude that MSAM1-92and MSAM1-94measured the same celestial signal.Subject headings:balloons —cosmic microwave background —cosmology:observations1.IntroductionMeasurements of anisotropy in the Cosmic Microwave Background Radiation(CMBR) continue as a subject of considerable interest to the astrophysics community.Future anisotropy measurements on scales of0.◦1to1.◦0will discriminate among early universe models and determine fundamental cosmological parameters(e.g.Hu and White1996, Knox1995and Jungman et al.1995).Measurements of anisotropy at angular scales near0.◦5have been reported recently by Ruhl et al.1995,Netterfield et al.1996,Gundersen et al.1995,and Tanaka et al.1995. Wilkinson1995voiced a common concern when he pointed out that“there are plausible systematic effects at levels comparable with the reported detections.”To address this concern the1994flight of the Medium Scale Anisotropy Measurement(MSAM1)observed the samefield as the1992flight to limit the possibility of systematic sources of the signal.Cheng et al.1994(hereafter Paper I)reported observations of anisotropy in the CMBR from thefirstflight of MSAM1in1992(MSAM1-92).Cheng et al.1996(hereafter Paper II)reported the results from the secondflight in1994(MSAM1-94).A conclusion of the latter is that while a quantitative comparison was pending,there was good qualitative agreement between the twoflights in the double difference data set,and that agreement was inconclusive for the single difference data set.This Letter presents a quantitative comparison of the MSAM1-92and MSAM1-94data sets.2.Instrument and ObservationsThe MSAM1instrument has been fully described in Fixsen et al.1996(hereafter Paper III);only an overview is given here.It is an off-axis Cassegrain telescope with a4-channel bolometric radiometer at the focus.The beamsize is28′FWHM and is moved ±40′on the sky by the nutating secondary.The radiometer has4frequency channels placed at5.7,9.3,16.5,and22.6cm−1.For these observation,emission in the lower two channels is dominated by the2.7K CMBR,while∼20K interstellar dust dominates the two higher channels.The instrument configuration was similar for the twoflights,with changes made only to the warm signal electronics and the gondola structure.These changes are discussed extensively in Paper III;the modifications to the electronics improved the noise performance, while those to the gondola reduced sidelobe sensitivity.The original superstructure had a large reflecting area above the beam,from which earthshine could potentially diffract into the beam.For the secondflight,the gondola was suspended by a cable system whichreduced the far-sidelobe response.The measured near sidelobe response dropped from−55dB in1992in the worst case to less than−75dB in all cases in1994.As described in Papers I and II,the observedfield is two strips at declination81.◦8±0.◦1, from right ascension15.h27to16.h84,and from17.h57to19.h71(all coordinates are J1994.5). Fig.1shows the weighted beam centers of thefields observed in the1992and1994flights.A CCD camera is used to determine absolute pointing for bothflights.Thefinal accuracy of the pointing determination is2.′5,limited by the gyroscope signal interpolation.This2.′5 uncertainty is small compared to the size of our beam(28′)and the bins(14′)used below, ensuring adequate alignment of the two datasets.During bothflights Jupiter was observed to calibrate the instrument and map the telescope beam.Beam maps and calibrations are done separately for the twoflights.The shape of the beam map is determined to4%of the maximum amplitude.Random noise in the gyroscope system contributes3.5%,and cosmic rays striking the detectors contribute 1.5%.Also,the choice of smoothing algorithm causes a1.5%systematic effbining this4%error from eachflight gives a5.8%relative calibration uncertainty.The uncertainty in Jupiter’s intrinsic brightness leads to an additional systematic uncertainty of10%for the results of eachflight;however,except for possible time variations in Jupiter’s brightness which we do not expect,this uncertainty does not contribute to the comparison of the two flights discussed here.3.Reanalysis of1992DataThe analyzed data sets reported in Papers I and II cannot be directly compared for two reasons:1)the boundaries of the sky bins are different,and2)the analysis reported in Paper I neglects correlations introduced by the removal of the small offset drift.The 1992data is reanalyzed to account for these correlations,using a procedure nearly identical to that of Paper II.The1994data is also reanalyzed,with differences from the original analysis noted in the text below.Here wefirst review the Paper II analysis,then note the differences between that and the reanalysis used here.First,the cosmic ray events are removed from the time stream.Cosmic ray removal techniques are different for the two years,and are discussed in Papers I and II.The data are then analyzed in a manner that provides sensitivity to two different angular scales on the sky.This is done by weighting the the time stream,S i,with one of two demodulation templates,d i,giving one“demodulated data point”,∆T cycle= i d i S i,for each full cycle of the secondary mirror movement.The“single difference demodulation”weights thesecondary-left data positively while weighting the secondary-right data negatively,giving a ∆T equal to the difference between the left and right temperatures.The result is a two lobed beam pattern on the sky with80′beam separation.The“double difference demodulation”weights the secondary-centered data positively,while weighting the secondary-left and secondary-right data negatively,giving a∆T equal to the difference between the center and the side temperatures.This produces a three lobed beam pattern on the sky,with40′beam separation.The single difference and double difference data are nearly statistically independent.A linear model isfit to these demodulated data including intensity for each sky bin and slow drifts in time.The noise used in thefit is estimated from the data.Both the time drift and noise estimate are described further below.The results of the linearfit are signal amplitudes for each sky bin with their associated covariances.A spectral model for each sky bin consisting of CMBR anisotropy plus emission from 20K Galactic dust,with emissivity proportional to frequency to the1.5power,isfit to all four frequency channels of binned sky data.The results of this spectralfit are the intensity of a“DUST”component and a“CMBR”component in each sky bin.The differences between the Paper II analysis and that done for this paper follow.This analysis uses a0.◦24bin size,double the size used in Paper II,which corresponds to the size of the central beam plateau.Angular orientation bins,which account for sky rotation relative to the secondary chop axis,are20◦,also double the previous size.The weighted beam centers of the identical bins are shown asfilled symbols in Fig.1.The noise estimates are formed from demodulated data.This is a change from Paper II, where the estimate is made after after having removed the drift model.The noise estimates are made separately for each minute of data by measuring the rms of the demodulated data in that minute.The new noise estimate is used in reanalyzing both the1992and1994 datasets.True sky signals make a negligible contribution to this rms estimate over these short time scales.This change has no substantial effect on the results of this Letter.Also,in Paper II the drift model included terms based on gondola sensors(air pressure, and the pitch and roll angles of the gondola outer frame).This model was used in the1994 reanalysis,while it was not used for the1992reanalysis.Instead,the original model for the drifts described in Paper I,a spline with knots every2.5minutes,was used.Fig. 1.—The weighted positions for each sky bin for both years.The triangles mark the 1992centers and the squares mark the1994centers.The declination scale has been greatly expanded relative to the RA scale in order to see the detailed pointing differences.Thefilled symbols are the weighted centers for the bins used in the comparison( δ =81◦50′).The bin boundaries(every0.◦24,or0.h11)in RA are not shown.The declination bin boundaries (every0.◦24)are marked by the horizontal lines.The angular orientation is ignored in this plot,but is not in our analysis.The vertical beam profile is plotted in the hatched region.Note that at this declination,every hour of RA corresponds to about2◦.parisonWe compare the signal measured at each point on the sky as measured in the twoflights,not just the rms levels of the sky signal found in each data set.In the1994flight, we attempted to observe the identical swath of sky observed in the1992flight.As can be seen in Fig.1,which is extremely enlarged in declination relative to right ascension,the 1994flight was low by about10′.To enable direct comparison,only the data from those bins which fall into the center declination bin is used.After this selection∼50%of the data is retained.The data from the1992flight is differenced from that of the1994flight to form a difference data set,92−94.Similarly,the two data sets are summed to form a sum data set,92+94.This is done for each demodulation and for both CMBR and DUST.To allow for differing offsets in the twoflights,a weighted mean is removed from each dataset.The covariance matrix,V ij,for both the sum and difference sets is the sum of the masked1992 and1994covariance matrices.There is no cross term because theflights have independent noise.The significance of any detected signal in the sum or difference is tested with aχ2 statistic,χ2±=ij (92±94)i V−1ij(92±94)j.Theχ2and degrees of freedom,and the cumulative probability,P(χ2),for the comparison is shown in Table1.P is the probability of getting a value ofχ2at or above the observed value,under the assumption that there is no signal in the data.This should be the case for the difference data,where the common sky signal should cancel.To check the effect of the relative calibration uncertainty onχ2,the1994dataset is rescaled by±6%and the value ofχ2recalculated.In all cases|∆χ2|≤2.A Kolmogorov-Smirnov(KS)test(Press et al.1992)of the92−94probabilities(.04, .22,.41,and.91)gives a74%probability that these are drawn from a uniform distribution from0to1.Based on this,we conclude that the92−94data in both the single and double difference demodulations for both the CMBR and DUST components is consistent with no observed signal.A KS test of the92+94probabilities(2×10−12,2×10−8,4×10−7,and1×10−4) gives a7×10−4probability that these are drawn from a uniform distribution from0to1. From this,together with the extremely lowχ2probabilities themselves,we see that there are statistically significant signals in all four92+94datasets.This result,combined with the absence of such signals in the92−94datasets,enables us to conclude that the signals observed during the twoflights are common,and therefore present on the sky.parison of1992and1994Data SetsType Data Setχ2/DOF PSingle DifferenceDouble Difference5.ConclusionsThe same region of the sky was observed in the1992and1994flights to confirm the detection of a celestial signal.It is clear from the statistical analysis that the same sky signal is measured in these twoflights.We conclude that at the level of our signal, our measurements are likely to be free from significant contamination from time-varying systematics such as sidelobe pickup or atmospheric contamination.In addition to our own confirmation of the MSAM1-92results,the Saskatoon experiment has recently observed this section of sky at lower frequencies,36GHz to46GHz (Netterfield et al.1996).They have compared their signal with the double difference CMBR signal from Paper I,andfind good agreement.This result,spanning nearly a decade in frequency,is strong evidence that we are observing CMBR anisotropies rather than some other astrophysical foreground source.We would like to thank E.Magnier,R.Rutledge,L.Knox,and A.Goldin for useful conversations.The research was supported by the NASA Office of Space Science, Astrophysics Division through grants NTG50720and50908and RTOP188-44.REFERENCESCheng,E.S.et al.1994,ApJ,422,L37.Cheng,E.S.et al.1996,ApJ,456,L71.Fixsen,D.J.et al.1996,ApJ.submitted,preprint astro-ph/9512006.Gundersen,J.O.et al.1995,ApJ,443,L57.Hu,W.and White,M.1996,ApJ.submitted,preprint astro-ph/9602019.Jungman,G.,Kamionkowski,M.,Kosowsky,A.,and Spergel,D.1995,Phys.Rev.D.submitted,preprint astro-ph/9512139.Knox,L.1995,Phys.Rev.D,52,4307.Netterfield,C.B.,Devlin,M.J.,Jarosik,N.,Page,L.,and Wollack,E.J.1996,ApJ.submitted,preprint astro-ph/9601197.Press,W.H.,Teukolsky,S.A.,Vetterling,W.T.,and Flannery,B.P.1992.Numerical Recipes in FORTRAN:The Art of Scientific Computing.Cambridge UniversityPress,Cambridge,2nd edition.Ruhl,J.E.,Dragovan,M.,Platt,S.R.,Kovac,J.,and Novak,G.1995,ApJ,453,L1. 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