Works matching DE "SPACE flight propulsion systems"
Results: 201
Research on Disturbance Compensation Control and Parameter Identification of a Multiple Air-Bearing Planar Air-Floating Platform Based on ADRC.
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- Aerospace (MDPI Publishing), 2025, v. 12, n. 2, p. 160, doi. 10.3390/aerospace12020160
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Evaluation and Performance Optimization of a Hydrogen Peroxide-Based Green Monopropellant Thruster for Steady-State Operations.
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- Aerospace (MDPI Publishing), 2025, v. 12, n. 2, p. 136, doi. 10.3390/aerospace12020136
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The Abracadabra of Engineering: Strong Structures from Flimsy Materials.
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- Technology Teacher, 2007, v. 66, n. 5, p. 17
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From Smoke Signals to Cell Phones: Tracing How Technologies Evolve.
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- Technology Teacher, 2002, v. 61, n. 7, p. 12
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First Example of 1,2,5‐Oxadiazole‐Based Hypergolic Ionic Liquids: A New Class of Potential Energetic Fuels.
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- Chemistry - A European Journal, 2023, v. 29, n. 44, p. 1, doi. 10.1002/chem.202300948
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Three-dimensional time optimal double angular momentum reversal trajectory using solar sails.
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- Celestial Mechanics & Dynamical Astronomy, 2011, v. 111, n. 4, p. 415, doi. 10.1007/s10569-011-9370-2
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Non-Keplerian orbits for electric sails.
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- Celestial Mechanics & Dynamical Astronomy, 2009, v. 105, n. 1-3, p. 179, doi. 10.1007/s10569-009-9200-y
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Artificial halo orbits for low-thrust propulsion spacecraft.
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- Celestial Mechanics & Dynamical Astronomy, 2009, v. 104, n. 4, p. 321, doi. 10.1007/s10569-009-9215-4
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Shear‐Induced Macropore‐Infused Nanocomposite Emulsion Thermosets (Adv. Mater. Interfaces 23/2022).
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- Advanced Materials Interfaces, 2022, v. 9, n. 23, p. 1, doi. 10.1002/admi.202270131
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Optimum preliminary design of ion thrusters in concurrent design facility.
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- Concurrent Engineering: Research & Applications, 2020, v. 28, n. 3, p. 189, doi. 10.1177/1063293X20938422
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Experimental Study on Ignition and Pressure-Gain Achievement in Low-Vacuum Conditions for a Pulsed Detonation Combustor.
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- Technologies (2227-7080), 2024, v. 12, n. 12, p. 252, doi. 10.3390/technologies12120252
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Optimizing Propellant Distribution for Interorbital Transfers.
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- Mathematics (2227-7390), 2024, v. 12, n. 6, p. 900, doi. 10.3390/math12060900
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A Liquid Launch Vehicle Safety Assessment Model Based on Semi-Quantitative Interval Belief Rule Base.
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- Mathematics (2227-7390), 2022, v. 10, n. 24, p. 4772, doi. 10.3390/math10244772
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Proposal of Specific Impulse Prediction Method for Bipropellant Thrusters.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2020, v. 63, n. 5, p. 189, doi. 10.2322/tjsass.63.189
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An Algorithm for Safe Landing of a Spacecraft during Descent from a Circumlunar Orbit.
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- Cosmic Research, 2022, v. 60, n. 5, p. 347, doi. 10.1134/S0010952522050082
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A Method for Solving the Multi-Extreme Problem of Optimizing Trajectories of a Spacecraft with an Elecrto-Jet Propulsion System's Thrust.
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- Cosmic Research, 2020, v. 58, n. 3, p. 192, doi. 10.1134/S001095252003003X
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Comparative Design and Ballistic Analysis of Using Chemical and Electric Propulsion Systems in the Solar Probe Project.
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- Cosmic Research, 2019, v. 57, n. 5, p. 325, doi. 10.1134/S0010952519050046
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Joint Optimization of Control and Main Trajectory and Design Parameters of an Interplanetary Spacecraft with an Electric Propulsion System.
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- Cosmic Research, 2019, v. 57, n. 3, p. 188, doi. 10.1134/S0010952519030079
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Analysis of the Structure of Families of Locally Optimum Solutions to the Problem of the Interplanetary Transfer of a Spacecraft with a Low-Thrust Engine.
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- Cosmic Research, 2018, v. 56, n. 5, p. 365, doi. 10.1134/S0010952518050076
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Analysis of the Requested Perfection of a Nuclear Electric Propulsion System for a Mars Mission with a 2-Year Duration.
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- Cosmic Research, 2018, v. 56, n. 5, p. 352, doi. 10.1134/S0010952518050039
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Designing corrections for the trajectory of the Spektr-R spacecraft in the event of immersions into the Moon's sphere of influence.
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- Cosmic Research, 2017, v. 55, n. 4, p. 290, doi. 10.1134/S0010952517040050
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Trajectory correction of the Spektr-R spacecraft motion.
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- Cosmic Research, 2014, v. 52, n. 5, p. 353, doi. 10.1134/S001095251405013X
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On a possibility of delivery of samples of primordial matter from asteroids of the main belt by a spacecraft with electric propulsion.
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- Cosmic Research, 2007, v. 45, n. 3, p. 210, doi. 10.1134/S0010952507030045
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Evolution of the Orbit of an Earth Satellite with a Solar Sail.
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- Cosmic Research, 2004, v. 42, n. 1, p. 79, doi. 10.1023/B:COSM.0000017565.85599.0b
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Experimental Flight of a Spacecraft with Solar Sail.
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- Cosmic Research, 2003, v. 41, n. 6, p. 612, doi. 10.1023/B:COSM.0000007961.72706.cd
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W and Re ion emitter-crowns and needles for μN space thruster elements manufactured by MIM.
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- Powder Metallurgy, 2015, v. 58, n. 4, p. 241, doi. 10.1179/0032589915Z.000000000241
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Performance Characteristics of Turkey's First 1,5 kW Hall Thruster Electric Propulsion System.
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- Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi, 2020, v. 13, n. 2, p. 155
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Optics: Taking wing on a beam of light.
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- Nature, 2010, v. 468, n. 7325, p. 734, doi. 10.1038/468734e
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Influence Parameter Analysis and Wrinkling Control of Space Membrane Structures.
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- Mechanics of Advanced Materials & Structures, 2010, v. 17, n. 1, p. 49, doi. 10.1080/15376490903082862
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Test particle acceleration in resistive torsional fan magnetic reconnection using laboratory plasma parameters.
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- Journal of Plasma Physics, 2021, v. 87, n. 6, p. 1, doi. 10.1017/S0022377821001203
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An Alfvenic reconnecting plasmoid thruster.
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- Journal of Plasma Physics, 2020, v. 86, n. 6, p. 1, doi. 10.1017/S0022377820001476
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Study of Manufacturing Processes for Liquid Rocket Turbopump Impellers: Test and Analysis.
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- Journal of Aerospace Technology & Management, 2020, v. 12, p. 1, doi. 10.5028/jatm.v12.1099
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Space Propulsion: a Survey Study About Current and Future Technologies.
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- Journal of Aerospace Technology & Management, 2018, v. 10, n. 1, p. 1, doi. 10.5028/jatm.v10.829
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Green Propellants: Oxidizers.
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- Journal of Aerospace Technology & Management, 2013, v. 5, n. 2, p. 139, doi. 10.5028/jatm.v5i2.229
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Development of Electric and ChemicalMicrothrusters.
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- International Journal of Aerospace Engineering, 2011, p. 1, doi. 10.1155/2011/361215
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Aerospace Engineer.
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- Science Teacher, 2013, v. 80, n. 1, p. 66
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Out of this world.
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- Sciences, 1999, v. 39, n. 6, p. 7
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- Article
Transient Flow in Porous Electrosprays.
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- Transport in Porous Media, 2024, v. 151, n. 12, p. 2277, doi. 10.1007/s11242-024-02113-9
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Combined Cycle Fatigue of Gas Turbine Blade Materials at Elevated Temperature.
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- Strain, 2010, v. 46, n. 4, p. 374, doi. 10.1111/j.1475-1305.2009.00666.x
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EFFECT OF THE HARTMANN NUMBER ON MHD STOKES FLOW IN A LID-DRIVEN CAVITY.
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- Magnetohydrodynamics (0024-998X), 2021, v. 57, n. 4, p. 423, doi. 10.22364/mhd.57.4.1
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REUSABLE AND LOW-COST SPACE ROCKET ENGINE WITH HIGH-EFFICIENT PROPELLANT PUMP.
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- Aerospace Research in Bulgaria, 2024, n. 36, p. 157, doi. 10.3897/arb.v36.e14
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Experimental Analysis of a Fixed-Wing VTOL MAV in Ground Effect.
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- International Journal of Micro Air Vehicles, 2010, v. 2, n. 1, p. 33, doi. 10.1260/1756-8293.2.1.33
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- Article
IN-VACUUM PHOTOGRAMMETRY OF A TEN-METER SQUARE SOLAR SAIL.
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- Experimental Techniques, 2006, v. 30, n. 3, p. 46, doi. 10.1111/j.1747-1567.2006.00042.x
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Darcy–Forchheimer MHD rotationally symmetric micropolar hybrid-nanofluid flow with melting heat transfer over a radially stretchable porous rotating disk.
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- Journal of Thermal Analysis & Calorimetry, 2024, v. 149, n. 24, p. 14625, doi. 10.1007/s10973-024-12986-z
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- Article
Thermal stability of hydroxylammonium nitrate (HAN).
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- Journal of Thermal Analysis & Calorimetry, 2017, v. 129, n. 2, p. 1083, doi. 10.1007/s10973-017-6287-3
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- Article
Magneto plasma sail formation reconfiguration around a heliocentric elliptic displaced orbit.
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- Astrophysics & Space Science, 2022, v. 367, n. 8, p. 1, doi. 10.1007/s10509-022-04105-x
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The influence of combustion efficiency on the characteristics of ramjets.
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- High Temperature, 2016, v. 54, n. 6, p. 882, doi. 10.1134/S0018151X16050047
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A Comprehensive Review of the Thermophysical Properties of Energetic Ionic Liquids.
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- Energies (19961073), 2025, v. 18, n. 2, p. 267, doi. 10.3390/en18020267
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- Article
Integrated Steady-State System Package for Nuclear Thermal Propulsion Analysis Using Multi-Dimensional Thermal Hydraulics and Dimensionless Turbopump Treatment.
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- Energies (19961073), 2024, v. 17, n. 13, p. 3068, doi. 10.3390/en17133068
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Optical Diagnostics for Solid Rocket Plumes Characterization: A Review.
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- Energies (19961073), 2022, v. 15, n. 4, p. 1470, doi. 10.3390/en15041470
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- Article