Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]
Chmielarek M +2 more
europepmc +1 more source
Improved simulation of cryogenic fluid mixing at supercritical pressures. [PDF]
Omair M, Akay HU.
europepmc +1 more source
Estimating CO2 emissions due to present and future suborbital space tourism industry. [PDF]
Huang AM, Xu Y.
europepmc +1 more source
Multimatrix Composite Materials for Rocket Nozzle Manufacturing: A Comparative Review. [PDF]
Meiirbekov M +7 more
europepmc +1 more source
Effect of Correlation on Multi-Engine Rocket Propulsion Systems [PDF]
A matter of great concern in the design and operation of multi-engine rocket propulsion systems is the effect of the premature shutdown of one engine on the vehicle.
Baker, J. R., Breneman, J. E.
core +1 more source
Using Hydrogen Peroxide for Rocket Fuel Tank Pressurization: Innovations, Advantages, and Challenges
This 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
doaj
Fault Detection and Isolation Based on Structural Analysis: Application to a Multi-Engine Propulsion Cluster. [PDF]
Murata R +4 more
europepmc +1 more source
Rocket injector anomalies study. Volume 1: Description of the mathematical model and solution procedure [PDF]
The capability of simulating three dimensional two phase reactive flows with combustion in the liquid fuelled rocket engines is demonstrated. This was accomplished by modifying an existing three dimensional computer program (REFLAN3D) with Eulerian ...
Przekwas, A. J. +2 more
core +1 more source
Advanced Nanomaterials and Energetic Application: Experiment and Simulation. [PDF]
Pang W, Trache D, Zhang K.
europepmc +1 more source
Influence of Adding Carbonaceous Fuels to Ionic Liquids on Propellant Properties. [PDF]
Gao X, Gao Z, Tan Y, Chen P, Du Z, Li Y.
europepmc +1 more source

