Results 221 to 230 of about 591 (257)

Combustion Diagnostics of Propellant with New Grain Geometries

1988
Abstract : High progressivity/density (HPD) propellants are under consideration at the Ballistic Research Laboratory (BRL) for a variety of enhanced ballistic applications. The HPD concept involves the tailoring of the mass generation rate to match the increasing chamber volume as the projectile moves down the gun tube.
A. A. Juhasz, K. J. White, R. E. Tompkins   +2 more
openaire   +1 more source

Recent Advances in Solid Propellant Grain Design

ARS Journal, 1959
s should be submitted to Meetings Manager, American Rocket Society, 500 Fifth Avenue, New York 36, N.Y. They will be for- warded to the appropriate Technical Committee Deadline date for abstracts is July 17.
openaire   +1 more source

Aging in Composite Propellant Grains

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2004
Gerhard Reeling Brouwer, Huub Keizers, Jim Buswell   +2 more
openaire   +1 more source

The Strain Analysis of Solid Propellant Rocket Grains

Journal of the Aerospace Sciences, 1960
There is often a wide divergence of interest between the missile engineer responsible for thrust performance on the one hand, and the motor tube manufacturer concerned with chemical composition on the other. The propellant grain design analj^st interested in structural integrity is, therefore, frequently hard put to compromise both aims efficiently in ...
openaire   +1 more source

NUMERICAL ANALYSIS OF GRAIN BURNBACK IN SOLID PROPELLANTS

International Journal of Energetic Materials and Chemical Propulsion, 2002
COLASURDO, GUIDO, CASALINO, LORENZO, PASTRONE, Dario Giuseppe, L. PIANTINO   +3 more
openaire   +5 more sources

Non-equilibrium heat exchange and multi-coupled nature of mass transfer in solvent removal of propellant grains

International Journal of Heat and Mass Transfer, 2022
Bao Rong
exaly  

Flame propagation into the crack of solid propellant grain

5th Propulsion Joint Specialist, 1969
openaire   +1 more source

MATHEMATICAL MODEL FOR PROPELLANT GRAIN GEOMETRY REGRESSION

Procceedings of the 19th Brazilian Congress of Thermal Sciences and Engineering, 2022
Leib Neubarth, Rachel Manhães de Lucena, Norberto Mangiavacchi, Daniel Chalhub, GIL ROBERTO VIEIRA. PINHEIRO, José da Rocha Miranda Pontes, Maurício Ferrapontoff Lemos, LAURILIO SILVA JUNIOR   +7 more
openaire   +1 more source

Solid rocket motor propellant grain burnback simulation based on fast minimum distance function calculation and improved marching tetrahedron method

Chinese Journal of Aeronautics, 2021
Jiani Li
exaly  

3-D grain burnback analysis of solid propellant rocket motors: Part 2 – modeling and simulations

Aerospace Science and Technology, 2008
A Ulas
exaly