Monoethanolamine-Based Fuels Hypergolic with Rocket-Grade Hydrogen Peroxide.
- Published in:
- Aerospace (MDPI Publishing), 2024, v. 11, n. 4, p. 309, doi. 10.3390/aerospace11040309
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- Article
Works matching Hydrogen peroxide rockets
Results: 12
1
2
The Influence of Thrust Chamber Structure Parameters on Regenerative Cooling Effect with Hydrogen Peroxide as Coolant in Liquid Rocket Engines.
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- Aerospace (MDPI Publishing), 2023, v. 10, n. 1, p. 65, doi. 10.3390/aerospace10010065
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- Article
3
Development of Green Storable Hybrid Rocket Propulsion Technology Using 98% Hydrogen Peroxide as Oxidizer.
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- Aerospace (MDPI Publishing), 2021, v. 8, n. 9, p. 234, doi. 10.3390/aerospace8090234
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- Article
4
HYPERGOLIC REACTION MECHANISMS OF CATALYTICALLY PROMOTED FUELS WITH ROCKET GRADE HYDROGEN PEROXIDE.
- Published in:
- Combustion Science & Technology, 2007, v. 179, n. 10, p. 2107, doi. 10.1080/00102200701386149
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- Article
5
High concentration hydrogen peroxide for rocket fuel applications.
- Published in:
- INCAS Bulletin, 2020, v. 12, n. 3, p. 151, doi. 10.13111/2066-8201.2020.12.3.12
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- Article
6
CoMn‐Spinel Oxides as Supported Catalyst for Rocket‐Grade Hydrogen Peroxide Decomposition.
- Published in:
- Propellants, Explosives, Pyrotechnics, 2020, v. 45, n. 10, p. 1627, doi. 10.1002/prep.202000020
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- Article
7
Hydrogen peroxide—a promising oxidizer for rocket engines: physical and chemical properties: decomposition in the liquid phase.
- Published in:
- Adsorption, 2024, v. 30, n. 8, p. 2187, doi. 10.1007/s10450-024-00547-7
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- Article
8
The design and performance on 200N-class bipropellant rocket engine using decomposed H<sub>2</sub>O<sub>2</sub> and Kerosene.
- Published in:
- INCAS Bulletin, 2019, v. 11, n. 3, p. 99, doi. 10.13111/2066-8201.2019.11.3.9
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- Article
9
Effect of High-Mass Fraction of Aluminum on Catalytic Hybrid Rocket Motor.
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- Applied Sciences (2076-3417), 2022, v. 12, n. 24, p. 13023, doi. 10.3390/app122413023
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- Article
10
Weltraumchemie: Antreiben, schützen, verbinden.
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- Nachrichten aus der Chemie, 2023, v. 71, n. 5, p. 26, doi. 10.1002/nadc.20234135332
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- Publication type:
- Article
11
Fuel Ignition in HTP Hybrid Rockets at Very Low Mass Fluxes: Challenges and Pulsed Preheating Techniques Using Palladium-Coated Catalysts.
- Published in:
- Aerospace (MDPI Publishing), 2024, v. 11, n. 11, p. 884, doi. 10.3390/aerospace11110884
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- Article
12
Experimental Investigation into Closed-Loop Control for HTPB-Based Hybrid Rocket Motors.
- Published in:
- Aerospace (MDPI Publishing), 2023, v. 10, n. 5, p. 421, doi. 10.3390/aerospace10050421
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- Publication type:
- Article