Results 201 to 210 of about 105,759 (263)

Analysis of laser backscattering from solid fuel rocket plumes

AIAA Journal, 1991
Analyses have been carried out for a ground-based experiment to measure laser backscattering from solid fuel rocket plumes. Mie scattering theory was used to compute the returned laser power as a function of range, wavelength, and scattering angle. The feasibility of retrieval of plume particle properties through various inversion methods was examined.
C. T. Christou, D. A. Levin
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Solid-Fuel Regression Rate Behavior of Vortex Hybrid Rocket Engines

Journal of Propulsion and Power, 2002
Aseriesofstaticenginee ringswereconductedtoinvestigatethesolid-fuelregressionratebehaviorandoperating characteristicsofvortexhybridrocketengines.Thevortexhybridenginecone gurationischaracterizedbyacoaxial, coswirling, countere owing vortex combustion e eld in a cylindrical fuel port.
William H. Knuth, Martin J. Chiaverini, J. Arthur Sauer, Daniel J. Gramer   +3 more
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Particulate Infrared Radiation in Aluminized Solid-Fuel Rocket Plumes

Journal of Spacecraft and Rockets, 1974
Strictly speaking, XB as derived, is the average frequency of event B where B = {one or more crashes during an independent subinterval of length ir}. We can write Eq.
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Experimental Investigation of Liquid Phase Breakup in Solid Fuel Rockets

Volume 1A, Symposia: Advances in Fluids Engineering Education; Turbomachinery Flow Predictions and Optimization; Applications in CFD; Bio-Inspired Fluid Mechanics; Droplet-Surface Interactions; CFD Verification and Validation; Development and Applications of Immersed Boundary Methods; DNS, LES, and Hybrid RANS/LES Methods, 2014
Solid rocket motors (SRM)s commonly use aluminized composite propellants. The combustion of aluminum composite propellants in SRM chambers lead to high temperature and pressure conditions resulting in the liquid alumina as a combustion product. The presence of liquid alumina in the flow presents problems such as; chemical erosion of propellant, and ...
Ryo S. Amano, Yi-Hsin Yen, Michael Hamman, Kristopher Rockey, Joshua Stangel   +4 more
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Mass Emissivity of Powder Gases in Solid Fuel Rockets

Journal of Applied Physics, 1948
An analysis has been carried out to determine an upper limit for the effective mass emissivity of the radiating gases in a solid fuel rocket motor. The calculations depend upon a comparison between experimentally observed performance data relating to a rocket motor and theoretical results based on a theory for the effect of radiation on the performance
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Finite acoustic oscillations and erosive burning in solid fuel rockets.

AIAA Journal, 1965
The acoustic combustion instability of a solid fuel rocket depends vitally on the response of the burning propellant surface to a sound field. The erosive part of this response can be significantly nonlinear at sound amplitudes too low in typical motors for ordinary second-order acoustic nonlinearities to be important. Then moderate amplitude phenomena
J. F. BIRD, R. W. HART, F. T. McCLURE
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Demonstration of Composite Hypergolic Solid Fuel for Hydrogen Peroxide Hybrid Rocket

AIAA SCITECH 2023 Forum, 2023
Junyeong Jeong, Seungho Lee, Sejin Kwon
semanticscholar   +1 more source

Three-dimensional numerical modeling of a rocket engine with solid fuel

Acta Astronautica, 2021
A. Kushnirenko, L. I. Stamov, V. Tyurenkova, M. Smirnova, E. Mikhalchenko   +4 more
semanticscholar   +1 more source

Effect of metal and metalloid solid-fuel additives on performance and nozzle ablation in a hydroxy-terminated polybutadiene based hybrid rocket motor

Aerospace Science and Technology, 2022
H. Tian, Z. Wang, Zihao Guo, Ruipeng Yu, Guobiao Cai, Yuanjun Zhang   +5 more
semanticscholar   +1 more source

Russian Solid-Fuel Rockets

Technology and Culture, 1968
G. A. Tokaty, V. N. Sokol'skii
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