標(biāo)題: Titlebook: Cryocoolers 13; Ronald G. Ross Conference proceedings 2005 Springer-Verlag US 2005 X-ray.development.modeling [打印本頁] 作者: Stimulant 時(shí)間: 2025-3-21 18:05
書目名稱Cryocoolers 13影響因子(影響力)
書目名稱Cryocoolers 13影響因子(影響力)學(xué)科排名
書目名稱Cryocoolers 13網(wǎng)絡(luò)公開度
書目名稱Cryocoolers 13網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Cryocoolers 13被引頻次
書目名稱Cryocoolers 13被引頻次學(xué)科排名
書目名稱Cryocoolers 13年度引用
書目名稱Cryocoolers 13年度引用學(xué)科排名
書目名稱Cryocoolers 13讀者反饋
書目名稱Cryocoolers 13讀者反饋學(xué)科排名
作者: exostosis 時(shí)間: 2025-3-21 22:10
Folkert Graafsma,Siddhartha Rajagopaling input power to the electronics. The total mass of the cooler and electronics system is less than 40 kg. The software driven control electronics provide the cooler control functions that are fully re-configurable and based on the NGST flight-qualified Advanced Cooler Electronics (ACE) with minor 作者: expire 時(shí)間: 2025-3-22 02:10
Conclusion and Further Research,lessons learned and performance achieved in the MIRI cryocooler application. In the final proposed configuration, all of the MIRI/JWST design considerations were successfully met. Although the cryocooler option was eventually deselected in favor of a solid-hydrogen stored cryogen system, the cryocoo作者: 打谷工具 時(shí)間: 2025-3-22 08:17 作者: AVANT 時(shí)間: 2025-3-22 08:48
The RTP Literature: Mind the Gap! View based control algorithm. In parallel to this effort, a manufacturing method was developed to enable production of very long continuous lengths of small bore finned tubing. This tubing is used in the highly effective recuperative heat exchanger associated with each stage of the cryocooler. A th作者: 寬容 時(shí)間: 2025-3-22 14:15 作者: 寬容 時(shí)間: 2025-3-22 19:37
The RTP Literature: Mind the Gap!ation problems due to outgassing has been diminished because the coils are not part of the helium circuit. Furthermore, all connections in the LSF95xx are laser-welded, which means that there is no additional locking required inside the cooler. By using a different magnet design, no magnet segments 作者: hidebound 時(shí)間: 2025-3-22 21:24 作者: anthesis 時(shí)間: 2025-3-23 02:37 作者: hidebound 時(shí)間: 2025-3-23 08:01 作者: ENDOW 時(shí)間: 2025-3-23 11:08
Cheng He,Yun-jin Yao,Xue-song Yeent sizing have been incorporated into this second generation design. The quantitative improvement provided by those design changes is presented. The second generation cold head design is currently being incorporated into a flight design warm-end expander motor assembly with Oxford-class flexure and作者: Orthodontics 時(shí)間: 2025-3-23 17:29 作者: CUB 時(shí)間: 2025-3-23 19:16
Ball Aerospace 4–10 K Space Cryocoolers under development for the NASA James Webb Space Telescope (JWST), Terrestrial Planet Finder (TPF), and Constellation X-Ray (Con-X) missions. The 4–10 K coolers are highly leveraged off previous Ball space coolers including multiple life test and flight units.作者: 胰臟 時(shí)間: 2025-3-24 00:52
NGST Advanced Cryocooler Technology Development Program (ACTDP) Cooler Systeming input power to the electronics. The total mass of the cooler and electronics system is less than 40 kg. The software driven control electronics provide the cooler control functions that are fully re-configurable and based on the NGST flight-qualified Advanced Cooler Electronics (ACE) with minor 作者: emulsify 時(shí)間: 2025-3-24 04:45
A Study of the Use of 6K ACTDP Cryocoolers for the MIRI Instrument on JWSTlessons learned and performance achieved in the MIRI cryocooler application. In the final proposed configuration, all of the MIRI/JWST design considerations were successfully met. Although the cryocooler option was eventually deselected in favor of a solid-hydrogen stored cryogen system, the cryocoo作者: 漂亮 時(shí)間: 2025-3-24 07:18 作者: 吃掉 時(shí)間: 2025-3-24 14:23
Development of a Small-Scale Collins-Type 10 K Cryocooler for Space Applications View based control algorithm. In parallel to this effort, a manufacturing method was developed to enable production of very long continuous lengths of small bore finned tubing. This tubing is used in the highly effective recuperative heat exchanger associated with each stage of the cryocooler. A th作者: PATRI 時(shí)間: 2025-3-24 17:18 作者: Mnemonics 時(shí)間: 2025-3-24 19:53 作者: Melodrama 時(shí)間: 2025-3-25 01:42 作者: FLIRT 時(shí)間: 2025-3-25 06:04 作者: TEM 時(shí)間: 2025-3-25 09:05
Lockheed Martin Two-Stage Pulse Tube Cryocooler for GIFTSripple suppression and vibration cancellation. The design is a “split” system in which the compressor and cold head are separated by a transfer line..The approach allows on orbit adjustment of the relative cooling loads and temperatures of the two stages..The controller provides precise temperature 作者: Ordnance 時(shí)間: 2025-3-25 14:49 作者: deadlock 時(shí)間: 2025-3-25 17:41 作者: abstemious 時(shí)間: 2025-3-25 22:15
Ball Aerospace 4–10 K Space Cryocoolersatures down to 10 K, Ball has developed long life Stirling cycle cryocoolers. For temperatures to 4 K and below, Ball has developed a hybrid Stirling/J-T (Joule-Thomson) cooler. The hybrid cooler has been verified in test to 3.5 K on a Ball program and a 6 K Development Model is in development on th作者: 解決 時(shí)間: 2025-3-26 03:25 作者: 鞭打 時(shí)間: 2025-3-26 04:53 作者: COMMA 時(shí)間: 2025-3-26 11:37 作者: intercede 時(shí)間: 2025-3-26 16:05
Status of Pulse Tube Cryocooler Development at Sunpowerd Space Flight Center. The first Phase II development effort between November 1999 and November 2001 established that a single-stage pulse tube driven by Sunpower’s manufactured linear compressor technology achieves efficient performance and promises to reach mass production costs similar to Sunpowe作者: panorama 時(shí)間: 2025-3-26 19:43
Development of a Small-Scale Collins-Type 10 K Cryocooler for Space Applicationsature levels ranging from 10K to 95K. A multi-stage 10K cryocooler is under development that applies microelectronic sophistication to achieve high efficiency in a reliable, compact design. The cryocooler is based upon a novel modification of the Collins cycle, a cycle commonly used in many high-eff作者: 小丑 時(shí)間: 2025-3-26 22:50
STI’s Solution for High Quantity Production of Stirling Coolersuctor (HTS) technology, STI has created a cryogenic receiver front-end (CRFE) used by major wireless operators to enhance their network performance. The “Sapphire” cryocooler is a key component in the STI SuperLink product family. Since 1999, more than 4,000 Sapphire cryocoolers have been deployed w作者: Deference 時(shí)間: 2025-3-27 03:51
Raytheon RS1 Cryocooler Performanceeon is currently manufacturing a low rate production lot of single-stage Stirling (RS1) cryocoolers to support its internal laboratory needs. The cryocooler features an Oxford-class design and is required to provide 3.3 W heat lift at 58K with an operational life in excess of 8 years. Initial testin作者: 宴會(huì) 時(shí)間: 2025-3-27 08:50 作者: 嘴唇可修剪 時(shí)間: 2025-3-27 11:13
Development of the LSF95xx 2nd Generation Flexure Bearing Coolerseries for cooling powers up to 3 W at 80 K and the LSF93xx series for cooling powers up to 8 W at 80 K. As a result of several design improvements, it was possible to decrease the length and mass of our flexure-bearing coolers. These improvements have been applied in the new LSF95xx series. With the作者: Lamina 時(shí)間: 2025-3-27 17:14 作者: 你正派 時(shí)間: 2025-3-27 18:19 作者: ORBIT 時(shí)間: 2025-3-27 21:58
Performance Test Results of a Miniature 50 to 80 K Pulse Tube Coolerd THALES Cryogenics. Prior to the EM manufacturing, a development phase was performed with an in-line architecture for the cold finger and using an existing flexure bearing compressor from THALES Cryogenics. The optimized development model pulse tube cooler demonstrated a cooling capacity of 1 W at 作者: 小鹿 時(shí)間: 2025-3-28 02:08
Performance of Japanese Pulse Tube Coolers for Space Applicationsure satellite applications. Three commercial samples were driven under vacuum conditions of below ～10. Pa. The cooling capacities, cooldown times, and the vibration generated by the cold heads and compressors were measured systematically. With room-temperature heat-sink conditions, the cooling capac作者: 歡騰 時(shí)間: 2025-3-28 06:16
High Capacity Staged Pulse Tubel planes and optics require cooling. The compressor is scaled from the High Efficiency Cryocooler compressor and is capable of using input powers up to 700 W. The two linear pulse tube cold heads are integrated with the compressor into an integral cryocooler. Provision is made to provide a thermal s作者: 受傷 時(shí)間: 2025-3-28 10:31 作者: 上坡 時(shí)間: 2025-3-28 15:51 作者: 柏樹 時(shí)間: 2025-3-28 19:22 作者: Cytokines 時(shí)間: 2025-3-28 23:16 作者: 溺愛 時(shí)間: 2025-3-29 06:19 作者: GEAR 時(shí)間: 2025-3-29 09:31 作者: 驚奇 時(shí)間: 2025-3-29 13:47
Status of Pulse Tube Cryocooler Development at Sunpowere tube cryocooler for cooling below 10 K..This paper reviews the development history of pulse tube technology at Sunpower Inc., updates the status of the single-stage pulse tube cryocooler, and presents the results of the three-stage pulse tube cryocooler development program.作者: 利用 時(shí)間: 2025-3-29 17:16 作者: cogent 時(shí)間: 2025-3-29 22:32 作者: Pepsin 時(shí)間: 2025-3-30 00:18
Ball Aerospace Next Generation 2-Stage 35 K SB235 Coolersck Sensor. A qualification unit SB235 was developed and has accumulated 2500 hours in a life test at the Air Force Research Laboratory (AFRL). The SB235 and its higher capacity derivative SB235E were designed for high cooling capacity, power and mass efficiency, and producibility for multiple unit build applications.作者: Oafishness 時(shí)間: 2025-3-30 07:09
High Capacity Staged Pulse Tubetrap between the cold heads in order to improve efficiency. The cooler is undergoing acceptance testing that includes thermal performance mapping over a range of reject temperatures and power levels, launch vibration testing and self induced vibration testing.作者: refraction 時(shí)間: 2025-3-30 11:49
The RTP Literature: Mind the Gap!g units currently in test providing insight to effects of screen packing densities, transfer line configuration and operational charge pressure. Good correlation of performance with the analytical model is demonstrated with some path for improvement identified. Life test update of legacy RS1 cryocooler designs is also provided.作者: flammable 時(shí)間: 2025-3-30 16:22
Research to Practice and Inclusionctured with a U-shaped architecture to provide a more compact cooler for improved integration. In this paper, thermal and mechanical test results for the new EM cooler are presented and analyzed for various heat sinking temperatures, input powers, and orientations.作者: 拋棄的貨物 時(shí)間: 2025-3-30 17:00
Lecture Notes in Electrical Engineeringr. The pulse tube refrigerators developed at Cryomech are expected to have mean time between maintenance (MTBM) > 5 years. The PT810s have been used for cryopumps and demonstrate their advanced features in the field.作者: exacerbate 時(shí)間: 2025-3-30 23:22 作者: 激勵(lì) 時(shí)間: 2025-3-31 01:40 作者: breadth 時(shí)間: 2025-3-31 08:52
Efficient 10 K Pulse Tube Cryocoolersr. The pulse tube refrigerators developed at Cryomech are expected to have mean time between maintenance (MTBM) > 5 years. The PT810s have been used for cryopumps and demonstrate their advanced features in the field.作者: evince 時(shí)間: 2025-3-31 09:55 作者: 伙伴 時(shí)間: 2025-3-31 15:44 作者: triptans 時(shí)間: 2025-3-31 18:59
CMC One-Watt Linear Cooler Performance Map at Higher Input Powerillustrates the mapping of a cryocooler performance envelope to determine the optimal operating point for this application. A key component of this performance map is CMC’s Linear Drive Cooler Electronics (LCDE). The versatility of the LCDE is demonstrated over the range of these tests.作者: 原告 時(shí)間: 2025-3-31 21:47 作者: 過時(shí) 時(shí)間: 2025-4-1 04:41 作者: surmount 時(shí)間: 2025-4-1 06:58
Expansion of Habitual Domains and DMCS,atures down to 10 K, Ball has developed long life Stirling cycle cryocoolers. For temperatures to 4 K and below, Ball has developed a hybrid Stirling/J-T (Joule-Thomson) cooler. The hybrid cooler has been verified in test to 3.5 K on a Ball program and a 6 K Development Model is in development on th作者: Debate 時(shí)間: 2025-4-1 13:42
Folkert Graafsma,Siddhartha Rajagopal is configured to provide remote cooling (12 m) at 18 and 6 K. The cooler is being developed under contract to the Jet Propulsion Laboratory with the objective of providing cooling for future NASA space observatory missions such as Terrestrial Planet Finder (TPF), Constellation X, and James Webb Spa作者: POWER 時(shí)間: 2025-4-1 17:15
Conclusion and Further Research,ar year 2003 an extensive study was carried out examining the application to this mission of hybrid 6K/18K J-T cryocoolers developed by NASA as part of their Advanced Cryocooler Technology Development Program (ACTDP). Among the most challenging requirements of the MIRI application were the requireme作者: 磨坊 時(shí)間: 2025-4-1 21:51
Expansion of Habitual Domains and DMCS,LM-ATC) is developing a four-stage pulse tube cryocooler and electronic controller to provide simultaneous cooling at 6 K and 18 K. LM-ATC successfully completed the design phase of the program, where a robust, simple pulse tube cryocooler system was designed to meet JPL’s cryocooler needs. The simp作者: indices 時(shí)間: 2025-4-1 23:20
