云南高校图书馆联盟文献共享服务平台- ROCKET

ROCKET: 作品数：358被引量：293H指数：8; 导出分析报告; 相关领域：航空宇航科学技术更多>>; 相关作者：乔庐峰雷思磊徐智勇经继松龚坚更多>>; 相关机构：北京理工大学解放军理工大学北京航空航天大学酒泉卫星发射中心更多>>; 相关期刊：更多>>; 相关基金：国家自然科学基金国家高技术研究发展计划国家教育部博士点基金上海市自然科学基金更多>>

新一代蜡油加氢处理催化剂RN-510的开发及工业应用: 《石油炼制与化工》2025年第2期8-12,共5页刘清河梁家林张璠玢杨清河胡志海; 中国石油化工股份有限公司合同项目(119006-3); 基于反应物分子与活性相最优匹配的新型催化剂制备技术平台(ROCKET+),成功开发了新一代高性能蜡油加氢处理催化剂RN-510。与RN-32V催化剂相比,RN-510催化剂的相对脱硫活性提高36%~54%,工业装填堆密度降低39%,同时催化剂的活性稳定性更高...; 关键词：失活 ROCKET^(+)技术高稳定性蜡油加氢处理脱硫脱氮

SCIENCE AND TECHNOLOGY: 《China Today》2025年第1期69-69,共1页; Long March 12 Makes Debut Flight from New Commercial Spaceport China successfully launched a new carrier rocket into space from the Hainan commercial spacecraft launch site in the southern island province of Hainan on...; 关键词：HAINAN ISLAND ROCKET

Effect of Free-Stream Mach Number on the Base Thermal Environment of LaunchVehicle: 《Journal of Thermal Science》2024年第6期2426-2436,共11页WANG Xu XU Xu YU Jiaqi YANG Qingchun; supported by the Outstanding Research Project of Shen Yuan Honors College;Academic Excellence Foundation of BUAA for PhD Students;National Key Laboratory of aerospace liquid propulsion; Convective heating of the rocket base caused by high-temperature reverse flow has long been a focus of thermal protection research.With distinctive structural characteristics,the base thermal environment of a twin-noz...; 关键词：rocket base heating free stream Mach number shock-turbulence interaction twin-nozzle

火箭风暴:2024 Triumph Rocket 3 Storm R: 《摩托车》2024年第10期50-55,共6页马文龙; 2020年,凯旋推出了巨无霸“火箭三缸”Rocket 3 R,以排量高达2458mL的水平并列三缸发动机震惊世人,当仁不让地成为最大的量产摩托车。4年过去了,“火箭三缸”依然是寂寞的王者。能超越“火箭三缸”的,只有“火箭三缸”的自我进化。2024...; 关键词：ROCKET 安全性能重磅出击自我进化摩托车风暴

Experimental investigation for temperature and emissivity by flame emission spectrum in a cavity of rocket based combined cycle combustor chamber: 《Defence Technology（防务技术）》2024年第9期114-122,共9页Weiguang Cai Shu Zheng Yan Wang Bing Liu Shaohua Zhu Li Zhao Qiang Lu; supported by the National Natural Science Foundation of China (Grant Nos.52276185,52276189 and 51976057);the Fundamental Research Funds for the Central Universities (Grant No.2021MS126);the Natural Science Foundation of Jiangsu Province (Grant No.BK20231209);the Proof-of-Concept Project of Zhongguancun Open Laboratory (Grant No.20220981113)。; Flame temperature and spectral emissivity were the important parameters characterizing the sufficient degree of fuel combustion and the particle radiative characteristics in the Rocket Based Combined Cycle(RBCC)combus...; 关键词：Rocket-based combined-cycle Supersonic combustion Flame temperature measurement EMISSIVITY Laser induced plasma combustion enhancement

Overview of CASC Space Launch Missions in 2024: 《Aerospace China》2024年第3期54-56,共3页; As the LM-3B carrier rocket successfully sent a communication technology test satellite into space on 20th December,the China Aerospace Science and Technology Corporation(CASC)has completed 51 launch missions for the ...; 关键词：LAUNCH ROCKET COMMUNICATION

SD-3 Carrier Rocket Successfully Launched 8 Satellites from Sea: 《Aerospace China》2024年第3期57-57,共1页; A Smart Dragon 3 carrier rocket launched from the waters near the city of Haiyang in East China’s Shandong Province on 24th September at 10:31 Beijing time,placing eight satellites including into planned orbit.SD-3 c...; 关键词：ROCKET LAUNCH ROCKET

Re-entry rocket basic flow characteristics and thermal environment of different retro-propulsion modes: 《Chinese Journal of Aeronautics》2024年第7期190-203,共14页Yifei SU Peijie SUN Yangwen CUI Guigao LE; co-supported by the National Level Project,China and Shanghai Municipal Major Science and Technology Project,China.In addition,the authors gratefully acknowledge the guidance on English writing and numerical methods of Professor Junfeng ZHANG from the Faculty of Engineering at Laurentian University.; During the supersonic re-entry of multi-nozzle heavy rockets into the atmosphere,the basic flow state becomes increasingly complex due to the coupling effect between the retropropulsion plumes and the freestream.A num...; 关键词：Re-entry rocket MULTI-NOZZLE Supersonic retro propulsion Thermal environment Afterburning effect

China Launches Chang’e 6 Probe Atop a LM-5 Carrier Rocket: 《Aerospace China》2024年第2期55-57,共3页; On May 3,a Long March 5 rocket carrying the Chang’e 6 probe blasted off from its launchpad at the Wenchang Space Launch Site at 17:27.The probe separated from the rocket and entered its planned transfer orbit shortly...; 关键词：LAUNCH ROCKET SEPARATED

China’s Reusable Carrier Rocket Completes First 10 km VTOL Test: 《Aerospace China》2024年第2期58-58,共1页; On June 23,2024,China completed the first 10 km-level VTOL flight test of the reusable launch vehicle at Jiuquan Satellite Launch Center,and the test mission was a complete success.This is the largest-scale VTOL fligh...; 关键词：VTOL ROCKET RETURN

ROCKET