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DS/EN 1829-1 - HIGH PRESSURE WATER JET MACHINES - SAFETY REQUIREMENTS - PART 1: MACHINES Organization: DS
Date: 2010-02-26
Description: This document applies to mobile and fixed high pressure water jet machines, in which the water pressure is generated by a pressure generator/pump and in which the maximum allowable working pressure is more than the upper limit fixed in the scope of EN 60335-2-79.
NBN - EN 1829-1 - HIGH PRESSURE WATER JET MACHINES - SAFETY REQUIREMENTS - PART 1: MACHINES Organization: NBN
Date: 2010-03-19
Description: This document applies to mobile and fixed high pressure water jet machines, in which the water pressure is generated by a pressure generator/pump and in which the maximum allowable working pressure is more than the upper limit fixed in the scope of EN 60335-2-79.
NBN - EN 1829-1 - HIGH PRESSURE WATER JET MACHINES - SAFETY REQUIREMENTS - PART 1: MACHINES Organization: NBN
Date: 2010-03-19
Description: This document applies to mobile and fixed high pressure water jet machines, in which the water pressure is generated by a pressure generator/pump and in which the maximum allowable working pressure is more than the upper limit fixed in the scope of EN 60335-2-79.
SNV - SN EN 1829-1 - HIGH PRESSURE WATER JET MACHINES - SAFETY REQUIREMENTS - PART 1: MACHINES Organization: SNV
Date: 2010-06-01
Description: This document applies to mobile and fixed high pressure water jet machines, in which the water pressure is generated by a pressure generator/pump and in which the maximum allowable working pressure is more than the upper limit fixed in the scope of EN 60335-2-79.
NBN - EN 1829-1 - MACHINES À JET D'EAU À HAUTE PRESSION - PRESCRIPTIONS DE SÉCURITÉ - PARTIE 1: MACHINES Organization: NBN
Date: 2010-03-19
Description: This document applies to mobile and fixed high pressure water jet machines, in which the water pressure is generated by a pressure generator/pump and in which the maximum allowable working pressure is more than the upper limit fixed in the scope of EN 60335-2-79.
SAE/TP - 2008-01-1959 - START-UP CHARACTERISTICS AND GRAVITY EFFECTS ON A MEDIUM/HIGH-LIFT HEAT PUMP USING ADVANCED HYBRID LOOP TECHNOLOGY Organization: SAE/TP
Date: 2008-06-29
Description: Thermal characterization was performed on a vapor compression heat pump using a novel, hybrid two phase loop design. Previous work on this technology has demonstrated its ability to provide passive phase separation and flow control based on capillary action.
SAE/TP - 2009-01-2437 - MARS SCIENCE LABORATORY MECHANICALLY PUMPED FLUID LOOP FOR THERMAL CONTROL – DESIGN, IMPLEMENTATION, AND TESTING Organization: SAE/TP
Date: 2009-07-12
Description: During operations on the surface of Mars this heat can be harnessed to maintain the rover and the science payload within their allowable limits during nights and winters without the use of electrical survival heaters. A mechanically pumped fluid loop heat rejection and recovery system (HRS) is used to pick up some of this waste heat and supply it to the rover and payload.
SAE/TP - 2008-01-2002 - DEVELOPMENT OF PASSIVELY ACTUATED THERMAL CONTROL VALVES FOR PASSIVE CONTROL OF MECHANICALLY PUMPED SINGLE-PHASE FLUID LOOPS FOR SPACE APPLICATIONS Organization: SAE/TP
Date: 2008-06-29
Description: To meet the thermal control requirements of the Mars Science Laboratory (MSL) rover, a splitting and a mixing thermal control valves with gradual control capabilities using a linear thermal actuator and a spool was developed at Jet Propulsion Laboratory (JPL). The key feature of these control valves is the balancing of the flow through the various branches of the fluid loop in order to balance the heat loads of the whole thermal system.
SAE/TP - 2007-01-3235 - MATHEMATICAL MODELING OF MULTIPLE EVAPORATOR / MULTIPLE CONDENSER LOOP HEAT PIPES AND TEST DATA VERIFICATION Organization: SAE/TP
Date: 2007-07-09
Description: NASA Goddard Space Flight Center in collaboration with NASA Jet Propulsion Laboratory recently proposed a miniature dual pump/condenser LHP system for use in future Mars missions.
SAE/TP - 2009-01-2419 - DESIGN DESCRIPTION AND INITIAL CHARACTERIZATION TESTING OF AN ACTIVE HEAT REJECTION RADIATOR WITH DIGITAL TURN-DOWN CAPABILITY Organization: SAE/TP
Date: 2009-07-12
Description: Sunada, Gajanana C. Birur and Jennifer R. Miller; Affiliation: Jet Propulsion Laboratory, California Institute of Technology Name: Ryan Stephan; Affiliation: NASA Johnson Space Center Meeting Details: Name: 39th International Conference on Environmental Systems Location: Savannah, Georgia, USA Date: 07-12-2009
HEI COMPLETE SET - COMPLETE SET OF HEI STANDARDS - CODE# 2948 Organization: HEI
Description: Complete Set of HEI Standards: Standards for Steam Surface Condensers, 11th Edition 2012 Standards for Direct Contact Barometric and Low Level Condensers, 8th Ed. 2010 Standards for Steam Jet Vacuum Systems 7th Edition 2012 Standards for Closed Feedwater Heaters, 8th Edition 2009 Standards and Typical Specifications for Tray Type Deaerators, 9th Edition 2011 Performance Standard for Liquid Ring Vacuum Pumps 4th Edition 2011 Standards for Shell & Tube Heat Exchangers, 5th Edition 2012 Standards for Air Cool Condensers, 1st Edition 2011 Standards for Gasketed Plate Heat Exchangers, 1st Edition 2014
ASME B19.1 - SAFETY STANDARD FOR AIR COMPRESSOR SYSTEMS Organization: ASME
Date: 1995-01-01
Description: Examples are truck air brake systems, aircraft air conditioning systems, and automotive emission control compressors; (e) thermal compressors such as steam jet ejectors; (f) turbochargers and superchargers that are part of a prime mover.
SAE AIR1191 - PERFORMANCE OF LOW PRESSURE RATIO EJECTORS FOR ENGINE NACELLE COOLING Organization: SAE
Date: 1999-03-01
Description: This device is also commonly called an eductor, an aspirator, or a jet pump. A straightforward method of defining the ejector geometry to provide the required cooling flow for a given application is needed.

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