Results 71 to 80 of about 1,551 (188)

Impact of Selected Metal Oxides on the Thermodynamics of Solid Rocket Propellant Combustion. [PDF]

Molecules
Janowska K, Waśkiewicz S, Skóra P, Hawelek L, Prasuła P, Jarosz T, Stolarczyk A.   +6 more
europepmc   +1 more source

Improving the Combustion Efficiency of Aluminum-Based Composite, Al@IL/FG, Through Surface Activation Reaction. [PDF]

Nanomaterials (Basel)
Zheng QL, Huang ZL, Xu HX, Li JZ, He W.
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

Simulating combustion flow in a rocket chamber

, 2008
Validerat; 20101217 (root)
openaire   +1 more source

Study on Creep Mechanical Properties of HTPB Solid Propellant. [PDF]

Materials (Basel)
Jin L, Jia S, Zhang Z, An Z, Lu Z.
europepmc   +1 more source

Acute toxicity of TNT derivatives and hydrazine-based compounds from explosive and rocket fuel contamination to darkling beetles (<i>Tenebrio molitor</i> and <i>Opatrum sabulosum</i>). [PDF]

PeerJ
Rybalka DF, Brygadyrenko VV.
europepmc   +1 more source

Advanced Nanomaterials and Energetic Application: Experiment and Simulation. [PDF]

Nanomaterials (Basel)
Pang W, Trache D, Zhang K.
europepmc   +1 more source

Design and Optimization of a Hybrid Gas Generator for Hydrogen Peroxide Tank Pressurization

Challenges and Issues of Modern Science
Purpose. This study develops a pressurization system for hydrogen peroxide tanks using a hybrid gas generator powered by liquid oxygen and solid fuel.
Mykhailo Vorobei, Mykola Bondarenko
doaj  

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

Enhanced Explosion Characteristics of Methane/Air Induced by Barium Nitrate under a Large Horizontal Pipeline. [PDF]

ACS Omega
Sun W, Chen Y, Li D.
europepmc   +1 more source