Results 151 to 160 of about 16,009 (301)
A Reliable Method for Predicting the Specific Impulse of Chemical Propellants
Journal of Aerospace Technology and Management, 2018 The specific impulse (Isp) is an important performance parameter that describes energy efficiency of propellant combustion and is intimately related to the rocket engine thrust.
Dany Frem
doaj
Performance Prediction of Liquid Rocket Thrust Chambers with Nonuniform Propellant Mixing
, 2006 openalex +2 more sources
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
Tank construction for space vehicles Patent [PDF]
, 1967 Liquid propellant tank design with semitoroidal ...
Blumrich, J. F., Loy, C. A.
core +1 more source
Forecasting thermoacoustic instabilities in liquid propellant rocket engines using multimodal Bayesian deep learning [PDF]
, 2022 Ushnish Sengupta +4 more
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RoBo6: Standardized MMT Light Curve Dataset for Rocket Body Classification [PDF]
arXivSpace debris presents a critical challenge for the sustainability of future space missions, emphasizing the need for robust and standardized identification methods. However, a comprehensive benchmark for rocket body classification remains absent. This paper addresses this gap by introducing the RoBo6 dataset for rocket body classification based on ...
arxiv
Study on Rheological Properties and Pouring Process of Hydroxyl-Terminated Polybutadiene (HTPB) Propellants. [PDF]
Polymers (Basel), 2023 Wang H, Ji Y, Jiang X, Li Z.
europepmc +1 more source
Nonlinear combustion instability in liquid-propellant rocket motors Quarterly report [PDF]
Fluid dynamic pancake model and droplet evaporation and combustion analysis related to nonlinear combustion instability in liquid propellant rocket ...
Burstein, S. Z., Chinitz, W.
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Supersonic-combustion rocket [PDF]
, 1973 A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy turbo pumps in a conventional rocket engine. The substitution results in a substantial reduction in rocket engine weight. The flame emanating from the small
Franciscus, L. C., Weber, R. J.
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