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SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
1999-01-1408
Micromachined Heat Sinks
 
981814
A Capillary Pump Loop Cooling System for the NICMOS Instrument
 
981543
Application of MIL-C-87252 in F-22 Liquid Cooling System
 
951400
Integrated Environmental Control System and Liquid Cooling System for F/A-18 E/F Aircraft
 
942176
Test Results of Reflux-Cooled Electromechanical Actuator
 
942177
VENTURI-FLOW COOLING SYSTEM: COMPARISON OF NUMERICAL AND EXPERIMENTAL RESULTS
 
932120
A Centrifugal Pump Concept Designed for Multiple Use in Space
 
932119
A Low Fin Height Heat Exchanger Technology Demonstrator for Hermes
 
932122
A Thermal Method for the Determination of Solar Absorptance and Thermal Emittance of Spacecraft Coatings
 
932239
CPHTS Hardware Development for the EOS AM Spacecraft Instruments
 
932306
Computer Model of Satellite Thermal Control System Using a Controlled Capillary Pumped Loop
 
932302
Design and Test of a Honeycomb Radiator Panel with Carbon Fiber Reinforced Plastic Facesheets and Aluminium Heat Pipes
 
932234
EOS AM Capillary Pumped Heat Transport System Development Testing Using TDM
 
932305
Experimental and Theoretical Investigation of Startup Regimes of Two-Phase Capillary Pumped Loops
 
932236
Flow Visualization within a Capillary Evaporator
 
932085
Global Reach, Global Power, A Goal Denied?
 
932303
High Capacity Grooved Heat Pipes
 
932084
High Heat Sink Fuels for Improved Aircraft Thermal Management
 
932086
Improving Aircraft Fuel-Thermal Management
 
932301
In-Orbit Demonstration of Two-Phase Heat Transport Technology: TPX/G557 Development & Pre-Launch Testing
 
932304
Investigation of the Heat Transfer Performance of a Capillary Pumped Ammonia Loop Under Gravity
 
932116
Porous Insulation Performance Under Martian Environment
 
932118
Sorption Refrigerators A Review of Current Development Status
 
932117
Survey and Evaluation of Multilayer Insulation Heat Transfer Measurements
 
932121
Technology Improvements to Optical Solar Reflectors
 
932235
Testing of Flight Components for the Capillary Pumped Loop Flight Experiment
 
932307
The Experience of Finite Elements Method Utilization for Simulation of Heat-Mass Transfer in Heat Pipes and Other Elements of Thermal Control Systems
 
932123
Thermal Control Coatings on Mg-Li Alloys
 
932237
Thermal Control Subsystem Design for the EOS Thermal Infrared Radiometer
 
931397
ADVANCED PASSIVE COOLING FOR HIGH POWER ELECTROMECHANICAL ACTUATORS
 
921941
A Thermal Management Assessment Tool for Advanced Hypersonic Aircraft
 
921944
Arterial Heat Pipe Performance in a Transient Heat Flux and Body Force Environment
 
921942
Evaluation of Cooling Concepts for High Power Avionics Applications
 
921943
Heat Transfer in Two-Dimensional Jet Impingement of a Dielectric Liquid on to a Flat Plate With Uniform Heat Flux
 
900965
Heating/Cooling with Polymeric Heat Exchangers
 
892316
Closed-System, High-Flux Evaporative Spray Cooling
 
871801
Flight Test Results for Several Light, Canard-Configured Airplanes
 
861724
Magnetic Refrigeration for Space Platforms
 
851856
ACTIVE CONTROL OF COMPRESSIBLE FLOWS ON A CURVED SURFACE
 
840940
The Closed-Loop Air-Cycle Option for Equipment Cooling on Aircraft
 
811083
High Speed VSCF Generator Design Consideration
 
801131
The All-Electric Airplane as an Energy Efficient Transport
 
670838
Design and Transient Performance of a Liquid Coolant System
 
660208
The Application of Vapor-Cycle Cooling Systems to Business Aircraft
 
650308
An Analytical and Experimental Study of the Vortex Subcooler — a New Concept in Mass Transfer Cooling
 
610437
COOLING FOR HYPERSONIC AIRCRAFT STRUCTURES
 

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