Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]
Chmielarek M +2 more
europepmc +1 more source
Boundary layer integral matrix procedure: Verification of models [PDF]
The three turbulent models currently available in the JANNAF version of the Aerotherm Boundary Layer Integral Matrix Procedure (BLIMP-J) code were studied.
Bonnett, W. S., Evans, R. M.
core +1 more source
Application of Gaussian SVM Flame Detection Model Based on Color and Gradient Features in Engine Test Plume Images. [PDF]
Yan S, Gao Y, Zhang Z, Li Y.
europepmc +1 more source
Advanced rocket propulsion [PDF]
Existing NASA research contracts are supporting development of advanced reinforced polymer and metal matrix composites for use in liquid rocket engines of the future.
Obrien, Charles J.
core +1 more source
Estimating CO2 emissions due to present and future suborbital space tourism industry. [PDF]
Huang AM, Xu Y.
europepmc +1 more source
Measurements for liquid rocket engine performance code verification [PDF]
The goal of the rocket engine performance code verification tests is to obtain the I sub sp with an accuracy of 0.25% or less. This needs to be done during the sequence of four related tests (two reactive and two hot gas simulation) to best utilize the ...
Palko, Richard L., Praharaj, Sarat C.
core +1 more source
Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine. [PDF]
Yu N +5 more
europepmc +1 more source
Modelling of heat addition to near-critical and supercritical fluids. [PDF]
Lamanna G, Steinhausen C.
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
In-situ propellant rocket engines for Mars mission ascent vehicle [PDF]
When comtemplating the human exploration of Mars, many scenarios using various propulsion systems have been considered. One propulsion option among them is a vehicle stage with multiple, pump fed rocket engines capable of operating on propellants ...
Roncace, Elizabeth A.
core +1 more source

