Thermophysics and Thermal ControlRaymond Viskanta |
From inside the book
Results 1-3 of 18
Page 231
... simulated the heat - transfer charac- teristics of one section of a grooved collector previously tested . The groove ... simulate the absorbed heat . The groove is placed in a wooden box ( length 157 cm , height 25 cm , width 29 cm ) and ...
... simulated the heat - transfer charac- teristics of one section of a grooved collector previously tested . The groove ... simulate the absorbed heat . The groove is placed in a wooden box ( length 157 cm , height 25 cm , width 29 cm ) and ...
Page 314
... simulated support attached . This support was made of polyethylene , and the thickness was selected to match the conductance of the flight - type fiberglass / epoxy support . After the simulated support was installed , the outer ...
... simulated support attached . This support was made of polyethylene , and the thickness was selected to match the conductance of the flight - type fiberglass / epoxy support . After the simulated support was installed , the outer ...
Page 436
... simulated probe enclosure volumes revealed film coefficients ranging from 0.5 to 2.0 Btu / hr - ft2- ° F for the ... simulate the internal dissipation of the actual equipment . Figures 12 and 13 show the TTM configuration . The 900 ° F ...
... simulated probe enclosure volumes revealed film coefficients ranging from 0.5 to 2.0 Btu / hr - ft2- ° F for the ... simulate the internal dissipation of the actual equipment . Figures 12 and 13 show the TTM configuration . The 900 ° F ...
Contents
Thermal Radiative Properties of Solar Sail Film Materials | 3 |
Infrared Reflectance and Refractive Index of Condensed Gas Films | 22 |
FarInfrared Properties of Baffle Coating Materials | 39 |
Copyright | |
14 other sections not shown
Common terms and phrases
AIAA aluminum analysis angle of attack Astronautics black epoxy paint blanket boundary calorimeter coating coefficient configuration constriction resistance contact area convection cooled correlation cryodeposits cryogen deposit thickness detector determined developed dimensionless dissimilar metal distribution emittance Engineering epoxy equation evaluated experimental film flight frit groove heat flow heat flux heat leak heat loss Heat Transfer heat-transfer heater increase insulation system integral integrating sphere Kapton laser load material MAWD measured microcontacts microsphere MLI system multilayer insulation NASA nodes obtained orbit parameters predicted presented pressure radiation radiative ratio refraction refractive index REYNOLDS ANALOGY sail sample shield shown in Fig solar absorptance solar sail solid Space spacecraft spectral reflectance sphere stainless steel substrate surface Table tank temperature thermal conductivity thermal contact conductance thermal control thermal performance thermocouples Thermophysics tion titania vacuum values view angle wall wavelength ZIRCALOY