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
- By:
- Publication type:
- Article
Works matching IS 22264310 AND DT 2019 AND VI 6 AND IP 12
Results: 10
1
2
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
- By:
- Publication type:
- Article
3
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
- By:
- Publication type:
- Article
4
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
- By:
- Publication type:
- Article
5
Integration and Verification Approach of ISTSat-1 CubeSat.
- Published in:
- Aerospace (MDPI Publishing), 2019, v. 6, n. 12, p. 131, doi. 10.3390/aerospace6120131
- By:
- Publication type:
- Article
6
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
- By:
- Publication type:
- Article
7
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
- By:
- Publication type:
- Article
8
Special Issue "Advances in Hybrid Rocket Technology and Related Analysis Methodologies".
- Published in:
- 2019
- By:
- Publication type:
- Editorial
9
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
- By:
- Publication type:
- Article
10
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
- By:
- Publication type:
- Article