Thermal Insulation Based on NBR-Elastomerized Phenolic Resin Reinforced with Carbon Fibers: Mechanical and Ablation Properties. [PDF]
Materials (Basel)Gržetić J +6 more
europepmc +1 more source
Development of microwave NDT inspection techniques for large solid propellant rocket motors Final report [PDF]
Microwave nondestructive testing techniques for large solid propellant rocket ...
Eckert, T. E., Lamb, B. L.
core +1 more source
IT modeling technologies of credible rocket propellants in liquid rocket engines processes [PDF]
, 2013 Р.Р. Назырова +1 more
openalex +1 more source
Mathematical model for heat transfer in variable thickness fins for rocket engines
Challenges and Issues of Modern SciencePurpose. This article aims to develop a mathematical model for a fin in the cooling system of liquid propellant rocket engines. The objective is to enable calculations for fins with arbitrary thickness variation. The developed mathematical model will be
Volodymyr Sliusariev, Valerii Bucharskyi
doaj
Theoretical stress mechanism and structural integrity of viscoelastic propellant grains with variable Poisson's ratio. [PDF]
Sci RepWang X +5 more
europepmc +1 more source
The hard start phenomena in hypergolic engines. Volume 1: Bibliography [PDF]
A bibliography of reports pertaining to the hard start phenomenon in attitude control rocket engines on Apollo spacecraft is presented. Some of the subjects discussed are; (1) combustion of hydrazine, (2) one dimensional theory of liquid fuel rocket ...
Miron, Y., Perlee, H. E.
core +1 more source
Performance Prediction of Liquid Rocket Thrust Chambers with Nonuniform Propellant Mixing
, 2006 openalex +2 more sources
Research on Time-Dimension Expansion of HBP Model Based on Hydroxyl-Terminated Polybutadiene (HTPB) Propellant Slurry. [PDF]
Polymers (Basel)Bai Y, Wang J, Feng Y, Cao P, Jiang X.
europepmc +1 more source
Thermophysical properties measurements and models for rocket propellant RP-1:
, 2007 Joseph W. Magee +9 more
openalex +1 more source
Study on elongation master curve of thermal aging composite modified double base propellant. [PDF]
Sci RepZheng J +8 more
europepmc +1 more source