Results 201 to 210 of about 16,009 (301)

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

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

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

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

Physical properties and thermodynamic characteristics of hydrogen. [PDF]

Heliyon
Levikhin AA, Boryaev АА.
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

Key attributes of nitrocellulose-based energetic materials and recent developments. [PDF]

Heliyon
Abdul Rahim KS, Samsuri A, Jamal SH, Mohd Nor SA, Rusly SNA, Ariff H, Abdul Latif NS.   +6 more
europepmc   +1 more source

Cryogenic propellant management in space: open challenges and perspectives. [PDF]

NPJ Microgravity
Simonini A, Dreyer M, Urbano A, Sanfedino F, Himeno T, Behruzi P, Avila M, Pinho J, Peveroni L, Gouriet JB.   +9 more
europepmc   +1 more source

Effect of aluminum and ammonium perchlorate particle sizes on the condensed combustion products characteristics of aluminized NEPE propellants. [PDF]

Sci Rep
Tu C, Chen X, Chen F, Zhuang Y, Cai W, Li Y, Li W, Zhou C, Xie R.   +8 more
europepmc   +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