Hybrid rocket combustion regression rate model.

AIAA Journal ◽  
1966 ◽  
Vol 4 (4) ◽  
pp. 752-753 ◽  
Author(s):  
EUGENE MILLER
Keyword(s):  
Rate Model ◽  
Hybrid Rocket ◽  
Regression Rate ◽  
Hybrid Rocket Combustion

scholarly journals Review of Classical Diffusion-Limited Regression Rate Models in Hybrid Rockets

Aerospace ◽  
2019 ◽  
Vol 6 (6) ◽  
pp. 75 ◽  
Author(s):  
Timothy Marquardt ◽  
Joseph Majdalani
Keyword(s):  
Radiation Effects ◽  
Hybrid Rocket ◽  
Physical Processes ◽  
Regression Rate ◽  
Rocket Motors ◽  
Diffusion Limited ◽  
Concise Review ◽  
Fluid Properties ◽  
Hybrid Rocket Combustion ◽  
Selection Of

In this article, we undertake a concise review of several milestone developments in classical regression rate models of hybrid rocket motors. After a brief description of the physical processes entailed in hybrid rocket combustion, Marxman’s diffusion-limited theory is re-constructed and discussed. Considerations beyond the scope of basic convection-driven models, which address disparate forms of the blowing correction, variable fluid properties, and pressure and radiation effects, are also given. Finally, a selection of kinetically-limited models is presented, with the aim of comparing the characteristics of several competing theories that become applicable under particular circumstances.

Regression-Rate and Heat-Transfer Correlations for Hybrid Rocket Combustion

2001 ◽  
Vol 17 (1) ◽  
pp. 99-110 ◽  
Author(s):  
Martin J. Chiaverini ◽  
Kenneth K. Kuo ◽  
Arie Peretz ◽  
George C. Harting
Keyword(s):  
Heat Transfer ◽  
Hybrid Rocket ◽  
Regression Rate ◽  
Hybrid Rocket Combustion ◽  
Heat Transfer Correlations

A Visual Study of the Combustion of High-Regression Rate and Classical Hybrid Rocket Fuels

2015 ◽  
Author(s):  
Elizabeth T. Jens ◽  
Victor A. Miller ◽  
Flora S. Mechentel ◽  
Brian J. Cantwell ◽  
Scott Hubbard
Keyword(s):  
Hybrid Rocket ◽  
Regression Rate ◽  
Visual Study
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