Results 71 to 80 of about 304 (185)

A Reliable Method for Predicting the Specific Impulse of Chemical Propellants

Journal of Aerospace Technology and Management, 2018
The specific impulse (Isp) is an important performance parameter that describes energy efficiency of propellant combustion and is intimately related to the rocket engine thrust.
Dany Frem
doaj  

Study on Rheological Properties and Pouring Process of Hydroxyl-Terminated Polybutadiene (HTPB) Propellants. [PDF]

Polymers (Basel), 2023
Wang H, Ji Y, Jiang X, Li Z.
europepmc   +1 more source

AN OPTIMIZED HYBRID ROCKET MOTOR FOR THE SARA PLATFORM REENTRY SYSTEM DOI 10.5028/jatm.2012.04032312

Journal of Aerospace Technology and Management, 2012
This paper has described a system design process, based on a multidisciplinary optimization technique, of a conceptual optimized hybrid propellant rocket motor. The proposed engine could be a technological option for the reentry maneuvering system of the
Pedro Luiz Kaled Da Cás, Cristiano Queiroz Vilanova, Manuel Nascimento Dias Barcelos Jr., Carlos Alberto Gurgel Veras   +3 more
doaj  

Influence of Adding Carbonaceous Fuels to Ionic Liquids on Propellant Properties. [PDF]

ACS Omega, 2022
Gao X, Gao Z, Tan Y, Chen P, Du Z, Li Y.
europepmc   +1 more source

Analysis of carbon nano particle variant as the propellant fuel to increase specific impulses of rockets. [PDF]

F1000Res, 2023
Navalino R, Muda N, Hafizah M, Ruyat Y.
europepmc   +1 more source

Combustion Simulation in Liquid-propellant Rocket Engine Development

Journal of the Visualization Society of Japan, 2021
Seiji TSUTSUMI, Takanori HAGA, Taro SHIMIZU   +2 more
openaire   +1 more source

Particle-Filter-Based Fault Diagnosis for the Startup Process of an Open-Cycle Liquid-Propellant Rocket Engine. [PDF]

Sensors (Basel)
Cha J, Ko S, Park SY.
europepmc   +1 more source

Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]

Polymers (Basel)
Chmielarek M, Szczęśniak B, Blacharski K.   +2 more
europepmc   +1 more source

A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. [PDF]

Sci Rep
Li T, He H, Yu N, Sun X, Cai G.
europepmc   +1 more source

Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine. [PDF]

Sci Rep, 2023
Yu N, Jiao B, Zhou C, Han S, Li T, Shi H.   +5 more
europepmc   +1 more source