Results 61 to 70 of about 2,824 (228)

LIQUID PROPULSION AT IAE: VISION OF THE ACTIVITIES AND FUTURE PERSPECTIVES. doi: 10.5028/jatm.2009.010199106

Journal of Aerospace Technology and Management, 2011
This paper presents the activities in the area of liquid propulsion, which received an effective boost at the end of the 90s.
Marco F. Carvalho Torres, Daniel Soares de Almeida, Yelisetty S. Rama Krishna, Luiz Silva, Wilson Kiyoshi Shimote   +4 more
doaj  

Viability of an Electrically Driven Pump-Fed Hybrid Rocket for Small Launcher Upper Stages

Aerospace, 2019
An electrically driven pump-fed cycle for a hybrid rocket engine is proposed and compared to a simpler gas-pressurized feed system. A liquid-oxygen/paraffin-based fuel hybrid rocket engine which powers the third stage of a Vega-like launcher is ...
Lorenzo Casalino, Filippo Masseni, Dario Pastrone   +2 more
doaj   +1 more source

Intelligent Fault Diagnosis of Liquid Rocket Engine via Interpretable LSTM with Multisensory Data. [PDF]

Sensors (Basel), 2023
Zhang X, Hua X, Zhu J, Ma M.
europepmc   +1 more source

Investigation of the cooling film distribution in liquid rocket engine [PDF]

Journal of Aerospace Technology and Management, 2011
This study presents the results of the investigation of a cooling method widely used in the combustion chambers, which is called cooling film, and it is applied to a liquid rocket engine that uses as propellants liquid oxygen and kerosene.
Luís Antonio Silva
doaj  

Analysis of low-thrust liquid rocket engines with a methane air pump unit

Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2016
The first airplane working on cryogenic fuel was developed in the USSR in early 1980s on the basis of the passenger aircraft Tu-154. It was then modified using a hydrogen engine installed instead of one of the three kerosene engines.
A. I. Ivanov, I. P. Kositsin, V. A. Borisov   +2 more
doaj   +1 more source

Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers. [PDF]

Data Brief, 2021
Pizzarelli M.
europepmc   +1 more source

Diversity of design knowledge for launch vehicle in view of fuels on hybrid rocket engine

Journal of Advanced Mechanical Design, Systems, and Manufacturing, 2014
A single-stage launch vehicle with hybrid rocket engine, which uses solid fuel and liquid oxidizer, has been studied and developed as a next-generation rocket for scientific observation due to the advantages as low cost, safety, re-ignition, and reduced ...
Kazuhisa CHIBA, Masahiro KANAZAKI, Masaki NAKAMIYA, Koki KITAGAWA, Toru SHIMADA   +4 more
doaj   +1 more source

Combustion Visualization and Liquid Jet in Crossflow Analysis of H₂O₂/Kerosene Bipropellant Thruster

Aerospace
In the H2O2/Kerosene bipropellant thruster, a liquid fuel jet is transversely injected into a crossflow of hot oxygen and water vapor, catalytically decomposed from a liquid oxidizer.
Suk Min Choi, Sangwoo Jung, Vincent Mario Pierre Ugolini, Sejin Kwon   +3 more
doaj   +1 more source

Conceptual design of single-stage launch vehicle with hybrid rocket engine using design informatics

Nihon Kikai Gakkai ronbunshu, 2014
A single-stage launch vehicle with hybrid rocket engine has been conceptually designed by using design informatics, which has three points of view, i.e., problem definition, optimization, and data mining.
Kazuhisa CHIBA, Shin'ya WATANABE, Masahiro KANAZAKI, Koki KITAGAWA, Toru SHIMADA   +4 more
doaj   +1 more source

Handbook of Recommended Practices for the Determination of Liquid Monopropellant Rocket Engine Performance, [PDF]

, 1979
R. A. Bjorklund, R. S. Rogero, R. K. Baerwald   +2 more
openalex   +1 more source