Works matching DE "SPACE vehicle design %26 construction"
Results: 109
Design and Build Your Own Spacecraft.
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- Technology Teacher, 2000, v. 60, n. 2, p. 15
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- Article
Solving a Spacecraft Design Problem.
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- Technology Teacher, 1998, v. 58, n. 4, p. 17
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- Article
X-ray Flare Spectra from the DIOGENESS Spectrometer and Its Concept Applied to ChemiX on the Interhelioprobe Spacecraft.
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- Solar Physics, 2015, v. 290, n. 12, p. 3683, doi. 10.1007/s11207-014-0644-1
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A method for calculating the resistance of spacecraft design elements under the action of space debris particles.
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- Cosmic Research, 2014, v. 52, n. 3, p. 229, doi. 10.1134/S0010952514020026
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The BDRG and SHOK instruments for studying gamma-ray burst prompt emission onboard the <i>Lomonosov</i> spacecraft.
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- Cosmic Research, 2013, v. 51, n. 6, p. 434, doi. 10.1134/S0010952513060014
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Vibration Antiresonance Design for a Spacecraft Multifunctional Structure.
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- Shock & Vibration, 2017, p. 1, doi. 10.1155/2017/5905684
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AERODYNAMIC AND THERMAL ENVIRONMENT OF A GAP UNDER HYPERSONIC FLIGHT.
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- Thermal Science, 2018, v. 22, n. 4, p. 1753, doi. 10.2298/TSCI1804753H
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Lockheed Martin Completes Major Design Review.
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- Microwave Journal, 2009, v. 52, n. 8, p. 39
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Lockheed Martin Achieves Key Milestones in Design Review Phase.
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- Microwave Journal, 2009, v. 52, n. 5, p. 141
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- Article
GEO-1 Spacecraft Ready for Environmental Test Phase.
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- Microwave Journal, 2008, v. 51, n. 6, p. 47
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- Article
Surrendering Outer Space.
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- Policy Review, 2009, n. 156, p. 55
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NASA to share telescope cost.
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- Nature, 2011, v. 476, n. 7361, p. 379, doi. 10.1038/476379a
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Space-science hopes rest on rocket test.
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- Nature, 2010, v. 465, n. 7296, p. 276, doi. 10.1038/465276a
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Mars mission delayed by concerns over reliability.
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- Nature, 2008, v. 456, n. 7223, p. 689, doi. 10.1038/456689b
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- Article
Vibration Evaluation of Wrinkled Membrane Inflated Beam.
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- Mechanics of Advanced Materials & Structures, 2015, v. 22, n. 5, p. 376, doi. 10.1080/15376494.2012.736062
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- Article
Deployment Dynamics for Solar Wings With Joint Friction.
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- Applied Mathematics & Mechanics (1000-0887), 2014, v. 35, n. 12, p. 1308, doi. 10.3879/j.issn.1000-0887.2014.12.003
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- Article
Spin-axis stabilisation of underactuated rigid spacecraft under sinusoidal disturbance.
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- International Journal of Control, 2008, v. 81, n. 12, p. 1901, doi. 10.1080/00207170801930217
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Our Future in the Stars.
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- Columbia Undergraduate Science Journal, 2015, v. 9, p. 6
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Modelling of Solar Radiation Pressure Effects: Parameter Analysis for the MICROSCOPE Mission.
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- International Journal of Aerospace Engineering, 2015, p. 1, doi. 10.1155/2015/928206
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Generating Solar Sail Trajectories in the Earth-Moon System Using Augmented Finite-DifferenceMethods.
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- International Journal of Aerospace Engineering, 2011, p. 1, doi. 10.1155/2011/476197
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Cascade-Based Controlled Attitude Synchronization and Tracking of Spacecraft in Leader-Follower Formation.
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- International Journal of Aerospace Engineering, 2011, p. 1, doi. 10.1155/2011/151262
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Benefits of Exergy-Based Analysis for Aerospace Engineering Applications--Part I.
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- International Journal of Aerospace Engineering, 2009, p. 1, doi. 10.1155/2009/409529
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UAVs Dynamic Mission Management in Adversarial Environments.
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- International Journal of Aerospace Engineering, 2009, p. 1, doi. 10.1155/2009/107214
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Aerospace Engineer.
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- Science Teacher, 2013, v. 80, n. 1, p. 66
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Career of the Month.
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- Science Teacher, 2007, v. 74, n. 7, p. 78
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Multidisciplinary design modeling and optimizationfor satellite with maneuver capability.
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- Structural & Multidisciplinary Optimization, 2014, v. 50, n. 5, p. 883, doi. 10.1007/s00158-014-1087-x
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Control-structure integrated multiobjective design for flexible spacecraft using MOEA/D.
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- Structural & Multidisciplinary Optimization, 2014, v. 50, n. 2, p. 347, doi. 10.1007/s00158-014-1053-7
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Principal angles between subspaces and reduced order modelling accuracy in optimization.
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- Structural & Multidisciplinary Optimization, 2014, v. 50, n. 2, p. 237, doi. 10.1007/s00158-013-1043-1
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- Article
Determination of realistic worst imperfection for cylindrical shells using surrogate model.
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- Structural & Multidisciplinary Optimization, 2013, v. 48, n. 4, p. 777, doi. 10.1007/s00158-013-0922-9
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KEEPING INFORMED: UPDATES ON MANAGEMENT.
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- Management Review, 1978, v. 67, n. 1, p. 4
- Publication type:
- Article
基于多体制的空天飞行器在轨相对 导航系统架构研究.
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- Computer Measurement & Control, 2018, v. 26, n. 5, p. 128, doi. 10.16526/j.cnki.11-4762/tp.2018.05.032
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面向批产化的小卫星自动化测试系统设计研究.
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- Computer Measurement & Control, 2018, v. 26, n. 2, p. 5, doi. 10.16256/j.cnki.11-4762/tp.2018.02.002
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FAILING TO LEARN? THE EFFECTS OF FAILURE AND SUCCESS ON ORGANIZATIONAL LEARNING IN THE GLOBAL ORBITAL LAUNCH VEHICLE INDUSTRY.
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- Academy of Management Journal, 2010, v. 53, n. 3, p. 451, doi. 10.5465/AMJ.2010.51467631
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Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach.
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- Modelling & Simulation in Engineering, 2014, p. 1, doi. 10.1155/2014/652571
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Survivability assessment of spacecraft impacted by orbit debris.
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- Defence Technology, 2021, v. 17, n. 3, p. 961, doi. 10.1016/j.dt.2020.06.003
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- Article
Extended state observer–based finite-time controller design for coupled spacecraft formation with actuator saturation.
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- Advances in Mechanical Engineering (Sage Publications Inc.), 2017, v. 9, n. 4, p. 1, doi. 10.1177/1687814017696413
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- Article
Reliability Analysis of a Filtering Reducer under the Discrete Space Environmental Shocks.
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- Advances in Mechanical Engineering (Sage Publications Inc.), 2014, p. 1, doi. 10.1155/2014/921720
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- Article
Development of an engineering methodology for non-linear fracture analysis of impact-damaged pressurized spacecraft structures.
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- Fracture & Structural Integrity, 2015, v. 9, p. 24, doi. 10.3221/IGF-ESIS.32.03
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- Article
Image-based spacecraft pointing model using single-bank dual-band registration.
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- International Journal of Remote Sensing, 2014, v. 35, n. 22, p. 7583, doi. 10.1080/01431161.2014.968986
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Being a Space Architect: Astrotecture™ Projects for NASA.
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- Architectural Design, 2014, v. 84, n. 6, p. 78, doi. 10.1002/ad.1836
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- Article
Impact detection and location for a plate structure using least squares support vector machines.
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- Structural Health Monitoring, 2014, v. 13, n. 1, p. 5, doi. 10.1177/1475921713495083
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- Article
Design of space thrusters: a topology optimization problem solved via a Branch and Bound method.
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- Journal of Global Optimization, 2016, v. 64, n. 2, p. 273, doi. 10.1007/s10898-015-0334-z
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- Article
A damage tolerance analysis for complex structures.
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- Archive of Applied Mechanics, 2016, v. 86, n. 4, p. 669, doi. 10.1007/s00419-015-1054-z
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- Article
Design Manufacture and Environmental Tests of Battery Pack for Spacecraft Freights.
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- International Journal of Advanced Design & Manufacturing Technology, 2016, v. 9, n. 3, p. 77
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- Article
Satellite Multidisciplinary Design Optimization Based on Support Vector Regression Surrogate Model.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2014, v. 46, n. 3, p. 481
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- Article
Unsteady Lifting Line Theory Using the Wagner Function for the Aerodynamic and Aeroelastic Modeling of 3D Wings.
- Published in:
- Aerospace (MDPI Publishing), 2018, v. 5, n. 3, p. 92, doi. 10.3390/aerospace5030092
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- Article
On the Wake Properties of Segmented Trailing Edge Extensions.
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- Aerospace (MDPI Publishing), 2018, v. 5, n. 3, p. 89, doi. 10.3390/aerospace5030089
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- Article
Computational Study of Propeller–Wing Aerodynamic Interaction.
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- Aerospace (MDPI Publishing), 2018, v. 5, n. 3, p. 79, doi. 10.3390/aerospace5030079
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- Publication type:
- Article
Transient Temperature Effects on the Aerothermoelastic Response of a Simple Wing.
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- Aerospace (MDPI Publishing), 2018, v. 5, n. 3, p. 71, doi. 10.3390/aerospace5030071
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- Publication type:
- Article
Development of Hollow Cathodes for Space Electric Propulsion at Sitael.
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- Aerospace (MDPI Publishing), 2017, v. 4, n. 2, p. 26, doi. 10.3390/aerospace4020026
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- Article