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Advanced planetary probe study. Volume 2 - Spin-stabilized spacecraft for the basic mission Final technical report

机译：先进的行星探针研究。第2卷 - 用于基本任务的旋转稳定航天器最终技术报告

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Spin-stabilized spacecraft design and functional requirements for Jupiter flyby mission in 1972 with 50-lb scientific payload

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年度 1966
页码 1-569
总页数 569
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ATLAS LAUNCH VEHICLES; CENTAUR LAUNCH VEHICLE; FLYBY MISSIONS; FUNCTIONAL DESIGN SPECIFICATIONS; INTERPLANETARY SPACECRAFT; JUPITER PROJECT; PAYLOADS; SPACECRAFT DESIGN; SPIN STABILIZATION; FLYBY MISSION; JUPITER PROJECT; PLANETARY SPACECRAFT; SPIN STABILIZATION;

机译：阿特拉斯发射车辆; CENTaUR LaUNCH VEHICLE;飞行任务;功能设计规格;行星际航天器; JUpITER项目;有效载荷;航天器设计;自旋稳定;飞行任务; JUpITER项目;行星航天器;自旋稳定;

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机译：用于行星科学仪器，航天器和任务的行星保护技术：NASA行星保护技术定义小组（PPTDT）的报告
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4. The Pennsylvania State University's Advanced Vehicle Team: EcoCAR3 Year One Final Technical Report [C] . Hugo H. McMenamin, Ryan Morris, Mohamed Wahba, IFAC Workshop on Engine and Powertrain Control, Simulation and Modeling . 2016

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6. 1160. CAUTIs are the Most Common Type of Healthcare-Associated Infection. In an Effort to Decrease CAUTI Rates Through Proactive Prevention We Sought to Develop a Weighted Model of CAUTI Risk Factors. The Final Set of Risk Factors Jointly Predicting CAUTI Were ADL Dependent CVA Catheter Replacement Within 7 days and Catheterization Duration ≥5. We Have Defined Contemporary Weighted Risk Factors for CAUTI and Intend to Utilize These to Deploy a Tiered Approach Where Patients with Risk Factors Will Receive Advanced in Addition to Basic Preventive Efforts [O] . Neha Nanda, Meline Aleksanyan -1

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7. Dynamic Isotope Power System (DIPS) Applications Study. Volume II. Nuclear Integrated Multimission Spacecraft (NIMS) design definition. Final report [O] . W. Z. Prickett 1979

机译：动态同位素电力系统（DIPS）应用研究。第II卷。核综合多次航天器（NIMS）设计定义。总结报告

Advanced planetary probe study. Volume 2 - Spin-stabilized spacecraft for the basic mission Final technical report

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