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Integrated model of a composite propellant rocket

AIP Conference Proceedings, 2016
The combustion of composite solid propellants was investigated and an available numerical model was improved for taking into account the change of pressure, when the process occurs in a confined environment, as inside a rocket. The pressure increase upon ignition is correctly described by the improved model for both sandwich and dispersed particles ...
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Review of composite propellant burn rate modeling

17th Aerospace Sciences Meeting, 1979
Steady-state combustion modeling of composite solid propellants is discussed with emphasis on the Beckstead-Derr-Price (BDP) model. The BDP model and some revisions are considered with respect to the analysis of monomodal ammonium perchlorate/inert binder propellants: topics examined include continuity relations, surface area relations, characteristic ...
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SYNOPTIC: Composite Propellant Combustion

AIAA Journal, 1970
R. L. DERR, J. R. OSBORN
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Modelling of Composite-Propellant Flames

2001
Abstract : We examined small deviations from axial symmetry in a solid-propellant rocket motor, and describe a 'bath-tub-vortex' effect, in which substantial axial vorticity is generated in a neighborhood of the chamber centerline. The unperturbed flow field is essentially inviscid at modest Reynolds numbers, even at the chamber walls, as has long been
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Validation of Composite Propellant Combustion Modeling Using Laminate Propellants

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2003
R. P. Fitzgerald, M. Q. Brewster
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Siloxane polyurethane composite propellant binders

AIAA Journal, 1970
J. M. HAMMOND   +2 more
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Research of composite propellants

Fuel and Energy Abstracts, 2001
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Aging in Composite Propellant Grains

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2004
Gerhard Reeling Brouwer   +2 more
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