Exaggerate
发表于 2025-3-27 00:32:43
1931-6828 st Design.•Low-Thrust Multi-Revolution Orbit Transfers.•Modeling and Optimization of Balance Layout Problems.•Pilot-Induced Oscillations Alleviation.•Modeling and Optimization of Hybrid Transfers to Near-Earth 978-3-319-82370-6978-3-319-41508-6Series ISSN 1931-6828 Series E-ISSN 1931-6836
盖他为秘密
发表于 2025-3-27 02:17:58
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Synovial-Fluid
发表于 2025-3-27 08:55:04
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adequate-intake
发表于 2025-3-27 10:23:13
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FLORA
发表于 2025-3-27 15:37:22
Re-entry Test Vehicle Configuration Selection and Analysis,es. Two fundamentally different vehicle shapes are considered, i.e., one based on a trapezoidal cross section and a sharp, water-cooled nose, for an increased lift-to-drag ratio, and one being a blunted bi-cone that is simple to manufacture, has good stability properties and good potentials for vari
朝圣者
发表于 2025-3-27 21:09:41
Optimal Robust Design of Hybrid Rocket Engines,ion procedure, and launcher performance are evaluated considering non-nominal regression rate correlations. The height of the attainable orbit results to be strongly jeopardized when the regression rate is larger than that of the nominal case (large oxidizer residual). In contrast, when regression r
Detonate
发表于 2025-3-28 01:45:47
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做作
发表于 2025-3-28 05:28:44
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性学院
发表于 2025-3-28 08:14:29
Probabilistic Safety Analysis of the Collision Between a Space Debris and a Satellite with an Islane parameters that, in case of bad estimation, tend to increase the collision probability value. This algorithm also gives an estimate of the collision probability maximum taking into account the likelihood of the parameters. The principles of this statistical technique are described throughout this
flaggy
发表于 2025-3-28 12:12:56
Book 2016r Regression Analysis in Space Engineering.•Regression-Based Sensitivity Analysis and Robust Design.•Low-Thrust Multi-Revolution Orbit Transfers.•Modeling and Optimization of Balance Layout Problems.•Pilot-Induced Oscillations Alleviation.•Modeling and Optimization of Hybrid Transfers to Near-Earth