Results 231 to 240 of about 573 (256)

Thermal stresses in a finite solid-propellant grain

2014
In order to gain a fundamental understanding of actual solid propellant thermal stress problems, the geometry of the solid propellant baa been idealized as a short, circular cylinder with flat ends. It is felt that the consideration of actual curved ends would only unduly have complicated the analysis. The method of solution for the thermal stresses in
openaire   +1 more source

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

Aerospace Science and Technology, 2008
A Ulas
exaly  

Estimation of location of defects in propellant grain by X-ray radiography

NDT and E International, 2008
Bikash Ghose
exaly  

A Geometry Independent Technique for Solid Propellant Grain Design

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 1996
N Ashgriz
exaly  

EXTRUSION TECHNIQUE FOR EXTRUDED COMPOSITE PROPELLANT GRAIN

International Journal of Energetic Materials and Chemical Propulsion, 2016
Ashwani K. Mishra, A. N. Patil, A. B. Dange, R. N. Patkar, P. K. Khanna, Seema D. Kakade   +5 more
openaire   +1 more source

REMOVED: Solid Propellant Grain Design

1993
openaire   +1 more source

Additive Manufacturing of Solid Rocket Propellant Grains

Journal of Propulsion and Power, 2018
Chandru, RA, Balasubramanian, Nikhil, Oommen, Charlie, Raghunandan, BN   +3 more
openaire   +1 more source

3-D grain burnback analysis of solid propellant rocket motors: Part 1 – ballistic motor tests

Aerospace Science and Technology, 2008
A Ulas
exaly  

Solid propellant grain

2019
MCBAIN ANDREW WILLIAM, WINGARD ZACHARY KEITH   +1 more
openaire   +1 more source

Method of manufacturing multi-layered propellant grains

2015
DURAND SIMON, PARADIS PIERRE-YVES, LEPAGE DANIEL   +2 more
openaire   +2 more sources