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Kühlkreislauf
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Launch Pad Closeout Operations for the Mars Science Laboratory's Heat Rejection System
High-altitude cooling I : resume of the cooling problem
Spacecraft engine thrust chamber cooling final report, 13 may 1963 - 12 apr. 1964
Devices for controlling thermal gradients in spacecraft structures
Measurement of Magnetostriction Between 4.2 and 77K
Navy Expeditionary Technology Transition Program (NETTP)
Analytical Study of Moderator Wall Cooling of Gaseous Nuclear Rocket Engines
A Vapour Cycle Cabin Cooling System for the Sea King MK. 50 Helicopter
Rocket Propulsion (RP) 21 Steering Committee Meeting - NASA Spacecraft Propulsion Update
A probe for total-enthalpy measurements in arcjet exhausts.
Evolvable Cryogenics (eCryo) Project Technology Workshop with Industry: Thermal Venting System (TVS)
Review of Flight Tests of NACA C and D Cowlings on the XP-42 Airplane
Heater Blanket, Battery, Morand Electronics Company - Types 1812 and 1813
Space Applications of Cryogenic Technology
High-altitude Cooling II : Air-cooled Engines
Review of flight tests of NACA C and D cowlings on the XP-42 airplane
Proceedings of the 2011 Space Cryogenics Workshop: Poised for the Future, Reflecting on the Past
Studying a Spacecraft Ventilation Fan: Progress and Possibilities
Long Term Life Testing of a Mechanically Pumped Cooling Loop for Spacecraft Thermal Control
Spacesuit Water Membrane Evaporator Integration with the ISS Extravehicular Mobility Unit
Investigation of Aircraft Heaters. 25 - Use of the Thermopile Radiometer
Cool the Force - Microclimatic Cooling Conference
Progress Report on the Development of Protected Construction for Hypersonic Vehicles
Nitrous oxide supercharging of an aircraft-engine cylinder
Type 50 Air Conditioner Truck. Part No. 1502858. Operation and Service Manual
Handbook of External Refrigeration Systems for Long Term Cryogenic Storage
A Feasibility Study of Heat-Pipe-Cooled Leading Edges for Hypersonic Cruise Aircraft
Advanced Propulsion with Onboard Power (APOP) Model Based Approach
Experimental Snow Plenum Air Cooling System for Byrd Station, Antarctica
Chamber Technology for Space Storable Propellants Final Report, Jun. 1964 - Sep. 1969
Contamination Level Evaluation of Spacecraft Air Conditioning System
Integrated Cryogenic System for Spacecraft Power, Thrust, and Cooling
Localized overheating in Aerobee regeneratively cooled thrust chambers
Advanced Space-Based Detector Research at the Air Force Research Laboratory