Found: 10
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Hardware-In-The-Loop and Software-In-The-Loop Testing of the MOVE-II CubeSat.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 130, doi. 10.3390/aerospace6120130
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- Publication type:
- Article
Influence of Polyisobutylene Kerosene Additive on Combustion Efficiency in a Liquid Propellant Rocket Engine.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 129, doi. 10.3390/aerospace6120129
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- Publication type:
- Article
Implementation and Hardware-In-The-Loop Simulation of a Magnetic Detumbling and Pointing Control Based on Three-Axis Magnetometer Data.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 133, doi. 10.3390/aerospace6120133
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- Publication type:
- Article
Determination of Serviceability Limits of a Turboshaft Engine by the Criterion of Blade Natural Frequency and Stall Margin.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 132, doi. 10.3390/aerospace6120132
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- Publication type:
- Article
Integration and Verification Approach of ISTSat-1 CubeSat.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 131, doi. 10.3390/aerospace6120131
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- Publication type:
- Article
Modelling of a Dual-Fuel-Mode Free-Jet Combustion System.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 135, doi. 10.3390/aerospace6120135
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- Publication type:
- Article
Assessment of a Turbo-Electric Aircraft Configuration with Aft-Propulsion Using Boundary Layer Ingestion.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 134, doi. 10.3390/aerospace6120134
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- Publication type:
- Article
Special Issue "Advances in Hybrid Rocket Technology and Related Analysis Methodologies".
- Published in:
- 2019
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- Publication type:
- Editorial
Nano-Sized and Mechanically Activated Composites: Perspectives for Enhanced Mass Burning Rate in Aluminized Solid Fuels for Hybrid Rocket Propulsion.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 127, doi. 10.3390/aerospace6120127
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- Publication type:
- Article
Predesign Considerations for the DC Link Voltage Level of the CENTRELINE Fuselage Fan Drive Unit.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 126, doi. 10.3390/aerospace6120126
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- Publication type:
- Article