Two-Stage Pulse Tube Cryocoolers for 4 K and 10 K Operation
Design and Characterization of a Miniature Pulse Tube Cooler
Technology Development Related to Tactical Cryocoolers at Raytheon Infrared Operations
A Hybrid, Multistage 10K Cryocooler for Space Applications
A Comparative Evaluation of Numerical Models for Cryocooler Regenerators
Oscillating Flow Characteristics of a Regenerator under Low Temperature Conditions
Study on Thermoacoustic DC-Flow Model for a Cyclic Regenerator due to Nonlinear Effects
Cooling Performance of a Small GM Cryocooler with a New Ceramic Magnetic Regenerator Material
Development of 40-80K Linear-Compressor Driven Pulse Tube Cryocoolers
An Experimental Study of the Phase Shift between Piston and Displacer in a Stirling Cryocooler
Continued Characterization Results for the Astrium 10K Developmental Cryocooler
Space Flight Qualification Program for the AMS-02 Commercial Cryocoolers
Development of a Low-Power Stirling Cycle Cryocooler for Space Applications
Study of a Vortex Tube by Analogy with a Heat Exchanger
LIGA-Fabricated High-Performance Micro-Channel Regenerators for Cryocoolers
MTTF Prediction in Design Phase on Thales Cryogenics Integral Coolers
Air Force Research Laboratory Space Cryogenic Technology Research Initiatives
High-Tc Squid-Based Gradiometer Cooled by a Cryotiger Gas-Mixture Cooler
Regenerator Characterization under Oscillating Flow and Pulsating Pressure
A First Order Model of a Hybrid Pulse Tube/Reverse-Brayton Cryocooler
Affecting the Gross Cooling Power of a Pulse Tube Cryocooler with Mass Flow Control
Development of a High Capacity Two-Stage Pulse Tube Cryocooler
Development of an Advanced Sorption Compressor and Its Application in a 125 K Cryocooler
Development Status of a 2.5 K - 4 K Closed-Cycle Cooler Suitable for Space Use
Test Results for the Single-Space Ball Flight Prototype Cooler
Sage: Object-Oriented Software for Cryocooler Design
Thermal Performance of Stirling-Cycle Cryocoolers: A Comparison of JPL-Tested Coolers
JPL Cryocooler Development and Test Program Overview
Development of a Stirling Cryocooler Using Hydrodynamic Gas Bearings
Space Cryogenic Refrigerator System (SCRS) Thermal Performance Test Results
Automated Closed-Cycle Cooling to 250 mK for the Polatron
Research on Adiabatic Capillary Tube Expansion Devices in Mixed-Refrigerant J-T Cryocoolers
Further Development of the Mixture Refrigeration Cycle with a Dephlegmation Separator
Regenerator Loss Measurements at Low Temperatures and High Frequencies