Using Hydrogen Peroxide for Rocket Fuel Tank Pressurization: Innovations, Advantages, and Challenges
Challenges and Issues of Modern ScienceThis paper explores the innovative use of hydrogen peroxide (H₂O₂) as a pressurizing agent for rocket fuel tanks, highlighting its potential to enhance efficiency and performance in rocket propulsion systems.
Mykhailo Vorobei, Mykola Bondarenko
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Thermal Insulation Based on NBR-Elastomerized Phenolic Resin Reinforced with Carbon Fibers: Mechanical and Ablation Properties. [PDF]
Materials (Basel)Gržetić J +6 more
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NUMERICAL MODELING OF COMBUSTION PROCESSES IN HYBRID ROCKET ENGINES
, 2016 Alessandro Mazzetti, Paolo Barbante
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Hybrid bearings for LH2 and LO2 turbopumps [PDF]
Hybrid combinations of hydrostatic and ball bearings can improve bearing performance for liquid hydrogen and liquid oxygen turbopumps. Analytic studies were conducted to optimize hybrid bearing designs for the SSME-type turbopump conditions.
Butner, M. F., Lee, F. C.
core +1 more source
Opposition-based chaotic evolution for optimization. [PDF]
Sci RepLi T, Pei Y.
europepmc +1 more source
Estimating CO2 emissions due to present and future suborbital space tourism industry. [PDF]
PLoS OneHuang AM, Xu Y.
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Audio-Based Engine Fault Diagnosis with Wavelet, Markov Blanket, ROCKET, and Optimized Machine Learning Classifiers. [PDF]
Sensors (Basel)Tuleski BL +4 more
europepmc +1 more source
Polymer-Based Thermal Protective Composites: The Role of Reinforcement and Matrix in Providing Strength and Fire Resistance. [PDF]
Polymers (Basel)Meiirbekov M +11 more
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Optimized Design of Sparse Antenna Array for 2D Subarrays Based on GA-PSO Algorithm and Ambiguity Function. [PDF]
Micromachines (Basel)Yang J, Lu J, Zhu T, Li C, Quan Y.
europepmc +1 more source
Analysis of a Hybrid Rocket Burn Using Generalized Compressible Flow
, 2015 Naveen Sri Uddanti
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