Procedures are given for formulating, blending, and applying MS-74 white thermal-control coating and CC-1 primer to spacecraft structures. Improved ultraviolet stability, higher emittance and low absorptivity, and enhanced adhesion characteristics result from the revised procedures
Spin resonance studies of zinc orthotitanate, synthesis of new pigments, and design of new test faci...
Many different passive thermal control materials were flown as part of the Materials on Internationa...
The potential of zinc orthotitanate as a pigment for spacecraft thermal control was demonstrated. Th...
Reactive encapsulation methods for thermal stabilization of zinc orthotitanate resin paints for spac...
Pigment manufacturing development, binder development, environmental effects evaluations, and genera...
The Air Force Space and Missile Systems Center and Wright Laboratory Materials Directorate (WL/ML) h...
A handbook of passive thermal control surfaces data pertaining to the heat transfer requirements of ...
Evaluating flight performance of Z-93 white paint in SERT 2 spacecraft thermal control system by cha...
Handbook of thermal design data and information on thermophysical properties of high performance ins...
The objective of significantly advancing the state-of-the-art of white, spacecraft-radiator coatings...
Thermal control coating degradation under vacuum and ultraviolet radiation by chemical change of pho...
Spacecraft radiators reject heat to their surroundings and coatings play an important role in this h...
Using zinc orthotitanate-pigmented potassium silicate paints for thermal control surface coating
Efforts to develop an engineering paint were concentrated on inorganic silicate-bonded systems as op...
Development of stable thermal control coatings with low solar absorptance to infrared emittance rati
Spin resonance studies of zinc orthotitanate, synthesis of new pigments, and design of new test faci...
Many different passive thermal control materials were flown as part of the Materials on Internationa...
The potential of zinc orthotitanate as a pigment for spacecraft thermal control was demonstrated. Th...
Reactive encapsulation methods for thermal stabilization of zinc orthotitanate resin paints for spac...
Pigment manufacturing development, binder development, environmental effects evaluations, and genera...
The Air Force Space and Missile Systems Center and Wright Laboratory Materials Directorate (WL/ML) h...
A handbook of passive thermal control surfaces data pertaining to the heat transfer requirements of ...
Evaluating flight performance of Z-93 white paint in SERT 2 spacecraft thermal control system by cha...
Handbook of thermal design data and information on thermophysical properties of high performance ins...
The objective of significantly advancing the state-of-the-art of white, spacecraft-radiator coatings...
Thermal control coating degradation under vacuum and ultraviolet radiation by chemical change of pho...
Spacecraft radiators reject heat to their surroundings and coatings play an important role in this h...
Using zinc orthotitanate-pigmented potassium silicate paints for thermal control surface coating
Efforts to develop an engineering paint were concentrated on inorganic silicate-bonded systems as op...
Development of stable thermal control coatings with low solar absorptance to infrared emittance rati
Spin resonance studies of zinc orthotitanate, synthesis of new pigments, and design of new test faci...
Many different passive thermal control materials were flown as part of the Materials on Internationa...
The potential of zinc orthotitanate as a pigment for spacecraft thermal control was demonstrated. Th...