Author: Henry C. HallerPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 44
Book Description
Heat-rejection and Weight Characteristics of Fin-tube Space Radiators with Tapered Fins
Author: Henry C. HallerPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 44
Book Description
Analysis of Heat-rejection Characteristics of Space Radiator Panels Utilizing Shared Fins
Author: Mario A. ColalucaPublisher:
ISBN:
Category : Continuum damage mechanics
Languages : en
Pages : 44
Book Description
NASA Technical Note
Author: Scientific and Technical Aerospace Reports
Author: Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1284
Book Description
Catalogue of Publications Issued by the Government of the United States
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1496
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1284
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1152
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1156
Book Description
Analysis of a Double Fin-tube Flat Condenser-radiator and Comparison with a Central Fin-tube Radiator
Author: Henry C. HallerPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 56
Book Description
An analytical study of a flat condenser-radiator with a double fin-tube geometry (closed sandwich) with variable tube side-wall thickness was performed for a Rankine space-power electric-generating system. The analysis of the double fin radiator included consideration of tube and header pressure drops, meteoroid protection for the tubes and headers, along with a detailed presentation of the heat rejection analysis and total weight characteristics. The double fin-tube radiator is compared to a conventional central fin-tube configuration on a heat rejection to weight basis for a four-panel radiator configuration. Both fin and tube geometries are compared on the basis of the same power level, working fluid temperature, tube and header pressure drop, radiator material, and meteoroid protection criteria. A beryllium radiator for a 1-megawatt system and a columbium alloy radiator for a 5OO-kilowatt system, both at a radiating temperature of 1700 R, were chosen for the weight and geometry comparison. The conclusion reached indicates a substantial weight savings can be realized with the double fin-tube arrangement if the tube side-wall thickness can be reduced as a result of a possible meteoroid bumper effect of the enclosing fins. Weight reductions compared to the central fin-tube geometry of up to 32 to 39 percent were shown to be possible for the maximum reduction in side- wall thickness in the two examples considered. This result further substantiated the preliminary conclusions given in an earlier reference that compared the double and central fin-tube configurations neglecting the effects of headers, pressure drops, tube wall temperature drop, and powerplant thermodynamic cycle considerations.