Results 151 to 160 of about 11,282 (264)

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

Anomaly Detection Method for Rocket Engines Based on Convex Optimized Information Fusion. [PDF]

Sensors (Basel)
Sun H, Cheng Y, Jiang B, Lu F, Wang N.
europepmc   +1 more source

Sensitivity-based state and parameter moving horizon estimation method for liquid propellant rocket engine

Z. Wang, Dan Wang, Hongyu Chen, Zhijiang Shao, Zhengyu Song   +4 more
openalex   +1 more source

About feasibility of SpaceX's human exploration Mars mission scenario with Starship. [PDF]

Sci Rep
Maiwald V, Bauerfeind M, Fälker S, Westphal B, Bach C.   +4 more
europepmc   +1 more source

Enhanced gas and plasticizer barrier HTPB composite liner implanted with parallel orientation Fe₃O₄/RGO nanosheets by an ultrasound/magnet-coassisted method. [PDF]

Ultrason Sonochem
Lu Z, Zhou Q, Zhang Y, Atya A, Zhang T, Zhang G, Zhang Y, Liu G, Jiang W, Hu Y.   +9 more
europepmc   +1 more source

Experimental Investigation of Liquid Diborane - Liquid Oxygen Propellant Combination in 100-pound-thrust Rocket Engine

, 1949
William H Rowe, P. M. Ordin, John M Diehl   +2 more
openalex   +1 more source

Rate-Dependent Tensile Properties of Aluminum-Hydroxide-Enhanced Ethylene Propylene Diene Monomer Coatings for Solid Rocket Motors. [PDF]

Materials (Basel)
Wang R, Zhang Y, Wang N, Wu Y.
europepmc   +1 more source

Pollution Effects and Management of Orbital Space Debris. [PDF]

ACS Omega
Shareefdeen Z, Al-Najjar H.
europepmc   +1 more source

Pair propellants analysis for liquid rocket engine using the energetic and mass comparison

, 2013
Fábio Rezende Prado dos Santos
openalex   +1 more source