نتایج جستجو برای: solid rocket motor

تعداد نتایج: 351579  

ژورنال: مواد پرانرژی 2013

Non-destructive testing methods are used to detecting defects in materials and evaluation of materials properties without causing changes to their usable properties. They are applied in industry to provide the assurance of high quality for semi-manufactured products, final products, devices and materials. Except of many civilian applications they are widely used in rocket and aviation industry ...

ژورنال: مواد پرانرژی 2015

HTPB based composite Solid propellants are the source of power for the propulsion of rockets and missiles. Since composite solid rocket propellants, used in rockets and missiles is the fastest degrading component of the complete system, shelf life of the system is mainly governed by the life of the propellants. During storage and transportation, the propellant grains are subjected to various co...

2013
Joshua A. Harris Ann Patterson-Hine

The Space Launch System is a Shuttle-derived heavy-lift vehicle currently in development to serve as NASA’s premiere launch vehicle for space exploration. The Space Launch System is a multistage rocket with two Solid Rocket Boosters and multiple payloads, including the Multi-Purpose Crew Vehicle. Planned Space Launch System destinations include near-Earth asteroids, the Moon, Mars, and Lagrange...

Journal: :The International Conference on Applied Mechanics and Mechanical Engineering 2016

ژورنال: مواد پرانرژی 2018

In this study, different flow analysis models in solid rocket motor are introduced. Amongst these models, some are not capable of predicting the effects of significant phenomena such as erosive burning and longitudinal acceleration. In order to consider these effects on the internal ballistic, a quasi-one-dimensional model was developed which employs generalized flow equations. A non-viscous an...

ژورنال: مواد پرانرژی 2019

Grain design is the most important part of solid rocket motor design. In this paper the goal is Finocyl grain design based on predetermined objective function with respect to Thrust history or Pressure history in order to satisfy various thrust performance requirements through an innovative design approach using Genetic algorithm optimization method. The classical sampling method is used for de...

Journal: :Problems of Mechatronics Armament Aviation Safety Engineering 2019

Journal: :TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 2019

This paper analyzes an induction motor with high temperature superconducter (HTS) coated slotted solid rotor. By slotting the solid rotor, the electromagnetic torque near synchronous speed will increase but the starting torque will decrease. To improve starting torque, rotor slots are coated with HTS materials. Using HTS material vary the rotor resistance to great extends in starting step and t...

Journal: :Acta Astronautica 2021

An innovative collection methodology based on a recently developed supersonic probe enabled the of alumina particulate from exhaust plume sub-scale solid propellant rocket motor and comparison with quench bomb analysis incipient agglomeration. Laser diffraction, scanning electron microscopy, X-ray spectroscopic methods were used to determine particle size, morphology, crystalline nature, elemen...

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