Results 271 to 280 of about 7,425 (303)
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Grain velocities during ignition of gun propellant

Combustion and Flame, 1975
Abstract By means of a dual-flash X-ray technique, propellant grain velocities during ignition have been determined for the Navy 5-in./38 gun. At the completion of ignition, the velocity profile along the grain bed is sharply peaked with maximun velocity at the propellant free surface.
openaire   +1 more source

Design and Analysis of Optimized Solid Propellant Grain

Lecture Notes in Mechanical Engineering
Mohammed Akbar   +1 more
exaly   +2 more sources

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   +2 more
openaire   +1 more source

Bulk Properties of Grain as Affected by Self-Propelled Rotational Type Grain Spreaders

Transactions of the ASAE, 1983
ABSTRACT A self-propelled rotational 4-trough grain spreader constructed at the U.S. Grain Marketing Research Laboratory and two commercially available rotational type grain spreaders were used to fill a 6.4-m diameter bin with wheat, corn, and grain sorghum. The grain for filling was choke-fed through an orifice to the spreaders.
null C. S. Chang   +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

On the dynamics of propeller-like dust grain in plasma

Physics of Plasmas, 2013
The equations of motion of a dust grain with non-spherical shape in plasma are generalized by incorporating the effects associated with propeller-like features of the grain's shape. For the grain shape close to rotationally symmetric, the stability of “stationary” (in terms of variables used in the grain dynamic equations) solutions are considered.
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 ...
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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
openaire   +1 more source

NUMERICAL ANALYSIS OF GRAIN BURNBACK IN SOLID PROPELLANTS

International Journal of Energetic Materials and Chemical Propulsion, 2002
COLASURDO, GUIDO   +3 more
openaire   +5 more sources

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