航空科学与技术(英文)最新文献_第3页

Mercuryplane—A Spacecraft for Regular Delivery of Astronauts onto the Mercury 水星飞机——定期向水星运送宇航员的航天器

航空科学与技术(英文) Pub Date : 2020-07-15 DOI: 10.4236/aast.2020.53005

A. Rubinraut

引用次数: 1

Empirical Patterns of High-Energy Particle Dynamics of the Van Allen Radiation Belts 范艾伦辐射带高能粒子动力学的经验模式

航空科学与技术(英文) Pub Date : 2020-06-23 DOI: 10.4236/aast.2020.52003

Yuhan Liu

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引用次数: 0

Thermodynamic Interpretation of Electron Density and Temperature Description in the Solar Corona 太阳日冕中电子密度和温度描述的热力学解释

航空科学与技术(英文) Pub Date : 2020-05-16 DOI: 10.4236/aast.2022.73010

D. Berdichevsky, J.M.G. G'omez, L. Vieira, A. D. Lago

{"title":"Thermodynamic Interpretation of Electron Density and Temperature Description in the Solar Corona","authors":"D. Berdichevsky, J.M.G. G'omez, L. Vieira, A. D. Lago","doi":"10.4236/aast.2022.73010","DOIUrl":"https://doi.org/10.4236/aast.2022.73010","url":null,"abstract":"We reach a thermodynamic interpretation of CODET model and its prediction to electrons density and temperature grounded on the physics of hydro magnetism in global equilibrium. The thermodynamic interpretation finds consistency with the model with a magneto-matter medium that is diamagnetic, in the context of ideal magnetohydrodynamics (MHD). It is further noticed that the CODET predicts a polytropic anomalous index for the electron gas of the Sun's corona. It is shown that this unusual characteristic is consistent with assuming that the low quiescent solar corona is a magneto-matter state which possesses an underlying structure that was earlier described to explain the 2-D adsorption process by a surface of a solid of molecules of a gas at a given temperature and pressure by Langmuir. In our case, it is assumed that we are in the presence of a 3-D similar coalescence process, i.e. a Langmuir amorphous lattice in thermodynamic equilibrium. In this way, constitutive properties of the medium magnetic permeability, the non-dispersive acoustic speed, the expected equilibration time for the 1.1 to 1.3$R_{odot}$, and energy density are determined quantitatively for most of the quiescent corona in a near solar minimum that extends for several months from 2008 to 2009.","PeriodicalId":61930,"journal":{"name":"航空科学与技术(英文)","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2020-05-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"45502642","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 0

A Unified Satellite Taxonomy Proposal Based on Mass and Size 基于质量和大小的统一卫星分类方案

航空科学与技术(英文) Pub Date : 2019-10-28 DOI: 10.4236/aast.2019.44005

C. Botelho, Ademir L. Xavier

引用次数: 4

Moonplane—A Spacecraft for Regular Delivery of Astronauts onto the Moon 月球飞机——定期向月球运送宇航员的航天器

航空科学与技术(英文) Pub Date : 2019-09-02 DOI: 10.4236/aast.2019.43004

A. Rubinraut

{"title":"Moonplane—A Spacecraft for Regular Delivery of Astronauts onto the Moon","authors":"A. Rubinraut","doi":"10.4236/aast.2019.43004","DOIUrl":"https://doi.org/10.4236/aast.2019.43004","url":null,"abstract":"A \u0000project of spacecraft “moonplane” for regular delivery of astronauts onto the \u0000Moon is considered. At the first stage of flight by using a carrier rocket, \u0000equipped with a chemical rocket engine, the astronauts are delivered on the \u0000international space station ISS. For flights from Earth orbit into Moon orbit, \u0000the design of a moonplane “MOND”, consisting of an interorbital module and a \u0000lunar module, has been developed. The interorbital module is an electric rocket, equipped with four \u0000superconductive magnetoplasma engine MARS. To power supply of the \u0000electromotors, a solar battery of gallium arsenide is used. The \u0000design of the lunar module with cabin astronauts, which is equipped with a chemical rocket engine for landing and take-off from \u0000the surface of the Moon, is developed. A method and a device for refuelling \u0000of the electrical rocket engines with nitrogen and for refuelling of the \u0000chemical rocket engines with oxygen and hydrogen, which are stored in cryogenic \u0000tanks of the moonplane in the liquid state is developed. \u0000The developed spacecraft is capable to regularly transport four \u0000astronauts off a moorage of ISS onto the surface of the Moon and back \u0000during 6 days. The total cost delivery of one astronaut is 4 million US \u0000dollars.","PeriodicalId":61930,"journal":{"name":"航空科学与技术(英文)","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2019-09-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"45852746","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 2

Elimination of the Potentially Dangerous Asteroid “Apophis” Using Electric Rocket 用电子火箭消除潜在危险小行星“阿波菲斯”

航空科学与技术(英文) Pub Date : 2019-06-12 DOI: 10.4236/AAST.2019.42002

A. Rubinraut

引用次数: 0

Predictive Control of Quad-Rotor Delivering Unknown Time-Varying Payloads Based upon Extended State Observer 基于扩展状态观测器的四转子传递未知时变有效载荷的预测控制

航空科学与技术(英文) Pub Date : 2019-06-11 DOI: 10.4236/AAST.2019.42003

Yuanyuan Wang

引用次数: 0

A Data-Driven Adaptive Method for Attitude Control of Fixed-Wing Unmanned Aerial Vehicles 固定翼无人机姿态控制的数据驱动自适应方法

航空科学与技术(英文) Pub Date : 2019-03-01 DOI: 10.4236/AAST.2019.41001

Meili Chen, Y. Wang

引用次数: 1