Results 181 to 190 of about 1,531,293 (230)

A critical review on prognostics for stochastic degrading systems under big data. [PDF]

Fundam Res
Li H, Si X, Zhang Z, Li T.
europepmc   +1 more source

Light-driven micro/nanobots. [PDF]

Nanophotonics
Vardhan RK, Kumar M, Xavier J.
europepmc   +1 more source

Vortex cooled thermoplastic chamber thruster for potential application to polymer based 3D printed space propulsion systems. [PDF]

Sci Rep
Aqailan M, Huh J.
europepmc   +1 more source

Evaluation of the Thermal Diffusivity of Carbon/Phenolic Composites (CPCs) through Oxy-Acetylene Torch (OAT) Test-Part 1: Experimental Characterization and Preliminary Validation. [PDF]

Polymers (Basel)
Natali M, Torre L, Rallini M.
europepmc   +1 more source

Environmental impact and sustainability of nanocellulose-based nitrated polymers in propellants. [PDF]

RSC Adv
Ahmad Aljafree NF, Norrrahim MNF, Samsuri A, Wan Yunus WMZ.   +3 more
europepmc   +1 more source

Probabilistic Damage Modeling and Thermal Shock Risk Assessment of UHTCMC Thruster Under Transient Green Propulsion Operation. [PDF]

Materials (Basel)
Jindal P, Doozandeh T, Botchu J.
europepmc   +1 more source

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Numerical modeling of hybrid rocket engine

Aerospace Systems, 2023
Anita Gehlot, Amit Kumar Thakur
exaly   +2 more sources

Hybrid rocket engines: The benefits and prospects

Aerospace Science and Technology, 2007
The review of research avenues for working processes (ignition, combustion, etc.) in hybrid rocket engines (HRE), for thermal protection and power characteristics is stated. Based on conducted design and exploratory studies and design developments, the reasonable fields of application of HRE to launch systems for orbit insertion of payload are ...
N.A. Davydenko, R.G. Gollender, A.M. Gubertov, V.V. Mironov, N.N. Volkov   +4 more
exaly   +2 more sources

Optimal propellant control in hybrid rocket engines

31st Joint Propulsion Conference and Exhibit, 1995
Paper AIAA 95 ...
COLASURDO, GUIDO, PASTRONE, Dario Giuseppe, CASALINO, LORENZO   +2 more
openaire   +3 more sources

Numerical investigations of hybrid rocket engines

Acta Astronautica, 2018
Abstract Paper presents the results of numerical studies of hybrid rocket engines operating cycle including unsteady-state transition stage. A mathematical model is developed accounting for the peculiarities of diffusion combustion of fuel in the flow of oxidant, which is composed of oxygen-nitrogen mixture.
V F Nikitin, V B Betelin, N N Smirnov
exaly   +2 more sources