Results 141 to 150 of about 25,209 (263)

Evaluation on the Regenerative Cooling Characteristics in Liquid Rocket Engine of 10tf-thrust using Kerosene and Liquid Oxygen as a Propellant

, 2004
Poong-Gyoo Han, Won-Kook Cho, Yong-Ho Cho   +2 more
openalex   +2 more sources

3 months transit time to Mars for human missions using SpaceX Starship. [PDF]

Sci Rep
Kingdon J.
europepmc   +1 more source

Fault Detection and Isolation Based on Structural Analysis: Application to a Multi-Engine Propulsion Cluster. [PDF]

Sensors (Basel)
Murata R, Marzat J, Piet-Lahanier H, Boujnah S, Belleoud P.   +4 more
europepmc   +1 more source

Bio-inspired multi-dimensional deep fusion learning for predicting dynamical aerospace propulsion systems. [PDF]

Commun Eng
Vergnolle MQ, Wu EZY, Sui Y, Wang Q.
europepmc   +1 more source

Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling

, 2014
A. G. Vorobiev, И. Н. Боровик, Song-Up Ha   +2 more
openalex   +2 more sources

Study on rheological properties of composite propellant slurry in the mixing process by using experimental and numerical simulation. [PDF]

RSC Adv
Guo Z, Fu X, Rossi R.
europepmc   +1 more source

Features of mathematical simulation of gas path dynamics in the problem of the stability of low-frequency processes in liquid-propellant rocket engines

, 2017
N. V. Khoriak, S. I. Dolhopolov
semanticscholar   +1 more source

Development of a mathematical model for the cooling channel of a liquid propellant rocket engine’s chamber with respect for variations in coolant density

Volodymyr Sliusariev, Valeriy Bucharskyi
openalex   +1 more source

Physical properties and thermodynamic characteristics of hydrogen. [PDF]

Heliyon
Levikhin AA, Boryaev АА.
europepmc   +1 more source

Research on Curing Reaction Kinetics and Curing Process of Nitrate Ester Plasticized Polyether (NEPE) Propellants. [PDF]

Polymers (Basel)
Wu Y, Guo Z, Yu H, Fu X.
europepmc   +1 more source