Results 21 to 30 of about 38,278 (273)
The process of fused deposition material (FDM) was used to manufacture propellant grains of Acrylonitrile Butadiene Styrene (ABS) as novel rocket fuel grain, with three types of geometry in the burning port.
Jose Alejandro Urrego +2 more
doaj +1 more source
Burnback Analysis of Solid Propellant Rocket Motors
42 pages, 20 figures, 2 ...
openaire +2 more sources
Estimation of internal ballistic parameters for the 107 mm rocket motor conceptual design
The demand for solid propellant rocket motors does not seem to fade, regardless of constant improvements in rocket technology. To make modifications that will result in improved design, it is crucial to use already existing motor models.
Ilma Subotic
doaj +1 more source
The Submerged Nozzle Damping Characteristics in Solid Rocket Motor
In this paper, the effects of the geometry of a submerged nozzle on the nozzle damping characteristics are studied numerically. Firstly, the numerical method is verified by the previous experimental data.
Xiaosi Li, Kai Pang, Xinyan Li
doaj +1 more source
Monte Carlo Uncertainty Quantification Using Quasi-1D SRM Ballistic Model
Compactness, reliability, readiness, and construction simplicity of solid rocket motors make them very appealing for commercial launcher missions and embarked systems. Solid propulsion grants high thrust-to-weight ratio, high volumetric specific impulse,
Davide Viganò +2 more
doaj +1 more source
The development of modern solid rocket technology with high-performance and high-loading ratio propellants places higher requirements on the safety and stability of the solid rocket motor.
Yin Zhang +6 more
doaj +1 more source
Solid Rocket Motor Design Using Hybrid Optimization
A particle swarm/pattern search hybrid optimizer was used to drive a solid rocket motor modeling code to an optimal solution. The solid motor code models tapered motor geometries using analytical burn back methods by slicing the grain into thin sections ...
Kevin Albarado +3 more
doaj +1 more source
A miniature solid propellant rocket motor [PDF]
A miniature solid-propellant rocket motor has been developed to impart a specific motion to an object deployed in space. This rocket motor effectively eliminated the need for a cold-gas thruster system or mechanical spin-up system. A low-energy igniter, an XMC4397, employing a semiconductor bridge was used to ignite the rocket motor.
M. Grubelich +5 more
openaire +1 more source
Parameters Affecting the Erosive Burning of Solid Rocket Motor
Increasing the velocity of gases inside solid rocket motors with low port-to-throat area ratios, leading to increased occurrence and severity of burning rate augmentation due to flow of propellant products across burning propellant surfaces (erosive ...
Abdelaziz Almostafa +2 more
doaj +1 more source
Steerable solid propellant rocket motor Patent [PDF]
Steerable solid propellant rocket motor adapted to effect payload orientation as multistage rocket stage or reduce velocity as ...
Raggio, C. W., Jr.
core +1 more source

