Works matching DE "SPACE vehicle design %26 construction"
Results: 109
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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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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X-ray work leading to Indian satellite launch.
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- Nature, 2001, v. 409, n. 6817, p. 126
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- Article
The design of an advanced primary deployment mechanism for a ...
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- Journal of Engineering Design, 1995, v. 6, n. 4, p. 291, doi. 10.1080/09544829508907919
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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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Unsteady Lifting Line Theory Using the Wagner Function for the Aerodynamic and Aeroelastic Modeling of 3D Wings.
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- Aerospace (MDPI Publishing), 2018, v. 5, n. 3, p. 92, doi. 10.3390/aerospace5030092
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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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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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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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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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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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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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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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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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On the Thermal Protection Systems of Landers for Venus Exploration.
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- Solar System Research, 2018, v. 52, n. 1, p. 37, doi. 10.1134/S0038094617060016
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Requirements for the appearance and basic design parameters of a micro-rocket system meant for launching nano-, pico, and femtoscale spacecraft.
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- Solar System Research, 2016, v. 50, n. 7, p. 477, doi. 10.1134/S0038094616070030
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Transformable descent vehicles.
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- Solar System Research, 2016, v. 50, n. 7, p. 489, doi. 10.1134/S0038094616070200
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Problems of design and development of advanced superheavy launch vehicles.
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- Solar System Research, 2016, v. 50, n. 7, p. 515, doi. 10.1134/S0038094616070042
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On the problem of designing small spacecraft with electric propulsion power plants for studying minor bodies of the Solar System.
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- Solar System Research, 2016, v. 50, n. 7, p. 533, doi. 10.1134/S0038094616070157
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The life of the Chief Designer of scientific robotic space systems-Georgii N. Babakin.
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- Solar System Research, 2015, v. 49, n. 7, p. 443, doi. 10.1134/S0038094615070114
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The development of the scientific and design school of G.N. Babakin during the creation of deep-space automated spacecraft.
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- Solar System Research, 2011, v. 45, n. 7, p. 563, doi. 10.1134/S0038094611070227
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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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ULTRA-HIGH TEMPERATURE CERAMIC COATINGS.
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- Advanced Materials & Processes, 2008, v. 166, n. 10, p. 30
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First JSF landing gear is shipped for CTOL variant.
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- Advanced Materials & Processes, 2005, v. 163, n. 9, p. 12
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EXTERNAL SPACE SHUTTLE TANK FOAM.
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- Advanced Materials & Processes, 2005, v. 163, n. 5, p. 27
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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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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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Space Fission Reactor Structural Materials: Choices Past, Present, and Future.
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- JOM: The Journal of The Minerals, Metals & Materials Society (TMS), 2007, v. 59, n. 4, p. 20, doi. 10.1007/s11837-007-0049-9
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Toucan Beaks Inspire Lightweight Materials.
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- JOM: The Journal of The Minerals, Metals & Materials Society (TMS), 2006, v. 58, n. 1, p. 8
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A Value-Centric Design and Certification Architecture for Space Systems.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 1, p. 1, doi. 10.2322/tjsass.62.1
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The Compatibility Evaluation Method of the 500N & 120N Japanese Bi-Propellant Thrusters with the HTV System & Operation Design.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 7
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SIB2/GSTOS Tools for Preparing Test Procedure - PlanEditor and SIB2Viewer.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 19
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Computational Analysis of Aerodynamic Performance of Mars Airplane.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
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Technical Challenges for Advanced Arcjets.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
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Analysis of Owl-like Airfoil Aerodynamics at Low Reynolds Number Flow.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 35
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New Procedure for Thermal Design of Micro- and Nano-satellites Pointing to Earth.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 11
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Skip Entry of a Capsule-type Manned Space Return Vehicle with Super-orbital Velocity.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 83
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Development and Evaluation of Small Size Whole Sky Observation Camera System for Micro-Satellite.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 27
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Evaluation of Crease Effects on Out-of-plane Stiffness of Solar Sails.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 107
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Ignition Probability Improvement of a Laser-Ignition Micro Solid Rocket.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 37
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Analysis of Knowledge Transfer Issues Relating to HTV Development.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 5
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Development of Main Propulsion System for Reusable Sounding Rocket: Design Considerations and Technology Demonstration.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
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Lessons from Space.
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- IEEE Software, 2011, v. 28, n. 6, p. 26, doi. 10.1109/MS.2011.143
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Automatic Checkout Equipment -- The Apollo Hippocrates.
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- Bulletin of the Atomic Scientists, 1969, v. 25, n. 7, p. 84, doi. 10.1080/00963402.1969.11455260
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THE LESSONS OF PROJECT MERCURY.
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- Bulletin of the Atomic Scientists, 1963, v. 19, n. 10, p. 51, doi. 10.1080/00963402.1963.11454587
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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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Aerospace Engineer.
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- Science Teacher, 2013, v. 80, n. 1, p. 66
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Coatings Technologies Bring NASA Solutions Down to Earth.
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- CoatingsTech, 2019, v. 16, n. 1, p. 18
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- Article