Dual solid cryogens for spacecraft refrigeration Patent
Dual solid cryogens for spacecraft refrigeration insuring low temperature cooling for extended periods
Engineering topics
Publications and source records attributed to Coston, R. M..
Dual solid cryogens for spacecraft refrigeration insuring low temperature cooling for extended periods
Design and construction of prototype spacecraft cryogenic refrigerator for infrared detector cooling
Solid cryogen refrigeration system for IR detector cooling in spacecraft applications
Thermal energy transport parallel to laminations in multilayer insulation without spacer material
High reliability solid cryogen refrigeration system consists of a container initially filled with a solid cryogen which is coupled thermally to an infrared detector by means of a link of high thermal conductivity extending from a heat exchanger within the cryogen container.
Temperature-dependent thermoconductivity of metal film on insulation laminations in relation to bulk parent material in insulation systems of cryogenic propellants
Diffusion coefficients, outgassing studies, and correlation of complete system thermal model computer program predictions with 82.6 inch tank test data
Temperature dependent thermoconductivity of metal film on insulation laminations in relation to bulk parent material in insulation systems of cryogenic propellants
Shingle attachment of multilayer insulation to cryogenic flight tanks
Transient gas-flow process in multilayer insulation systems during evacuation predicted by equations in conjunction with measured permeabilities and diffusion coefficients
Hydrogen vapor barrier materials measuring permeation rates, contraction and tensile properties from room to cryogenic temperatures