## An uncertainty analysis for satellite calorimetric measurements |

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absorptance of sensor AIAA albedo input Ames Research Center ANALYSIS FOR SATELLITE appendix as(Fs+ Faa aT4-FpP aTi4 ccg/e common base plate Conditions for solution derivatives were developed design guides developed with respect Dimensionless Dimensionless dT A d0 dT d0 e2FpP+ e2S(Fs+Faa earth radiation effect of uncertainty eliminated by virtue energy equation entrance into sunlight Faa)S eliminated Fp(e FpP eliminated Fs+ Faa)S heat capacity heat leak i e Fs+Faa independent variables involving infrared emittance ratio magnitude Moffett Field optically black Orbit time measured OSO-III overall uncertainty Partial derivatives planet planetary infrared radiation radiant flux S(FS S(FS+Faa SATELLITE CALORIMETRIC MEASUREMENTS satellite entrance sensor surface sets of independent simplified by writing simultaneous solution single temperature measurement Solar absorptance Solar constant T-Tb test surface uncertainty analysis v2FpP variables involving temperature vFpP View factors virtue of simultaneous wc _d_ wc d dT wc dT