Results 91 to 100 of about 2,583,997 (256)

Solid rocket propulsion [PDF]

open access: yes, 1991
The solid rocket motor failure database; current programs; and shortfalls of solid rocket propulsion are examined.
Nichols, Ronald L., Clinton, C.
core  

Supporting Young Foreign Language Learners With Image Generative AI in Digital Multimodal Composing: Benefits and Challenges

open access: yesTESOL Quarterly, EarlyView.
Abstract Integrating generative artificial intelligence (GenAI) into digital multimodal composing (DMC) offers promising avenues for young Foreign Language (FL) learners' learning experiences. Image‐based GenAI tools enable students to generate personalized images from written prompts to help convey meanings, and DMC combines text, images, and sound to
Alex Lap‐kwan Lam
wiley   +1 more source

Large‐Scale Applications of Plasma Technologies: Progresses and Challenges

open access: yesHigh Voltage, EarlyView.
ABSTRACT Plasma technologies convert electrical power into energetic electrons, ions, reactive species, radiation and heat, thereby breaking through the bottleneck of purely thermal or chemical routes and bringing impressive changes to our world. This roadmap reviews the progress and challenges of plasma technologies from a large‐scale and application ...
Pankaj Attri   +51 more
wiley   +1 more source

Design and fabrication of a solid rocket motor [PDF]

open access: yes, 2013
Rocket have been used from as early as the thirteenth century as fireworks and weapon. However, since then the usage of the rocket have been diversified.
Wan Nursyazwani, Ibrahim
core   +2 more sources

Chemically Collapsible Mandrel for Solid Rocket Motor Processing

open access: yesJournal of Aerospace Technology and Management, 2015
Composite propellant mainly consists of two parts, binder matrix (prepolymer, plasticizer, cross linker, antioxidant and curative etc.) and solid ingredients (oxidizer, metal fuel, burn rate modifier, combustion stabilizer etc.).
Abhijit Dey   +3 more
doaj  

A Study on the Influence of Flight Parameters on Two-Phase Flow and Radiation in the Plume of Solid Rocket Motors

open access: yesAerospace
Based on a pre-constructed simplified chemical reaction mechanism for afterburning in exhaust plumes, this study integrates a gas–solid two-phase combustion flow model with numerical radiative transfer calculations to systematically explore the ...
Moding Peng   +4 more
doaj   +1 more source

Numerical simulation of cook-off characteristics for AP/HTPB

open access: yesDefence Technology, 2018
The present study is devoted to researching the thermal security problems of large-scale solid rocket motor with Ammonium perchlorate/Hydroxyl-terminated polybutadiene (AP/HTPB). A two-dimensional axisymmetric model for the cook-off of solid rocket motor
Qing Ye, Yong-gang Yu
doaj   +1 more source

VOID URBANISM: Unbuilt New Cities and State Formation in the Democratic Republic of Congo

open access: yesInternational Journal of Urban and Regional Research, EarlyView.
Abstract Based on an analysis of the planning process behind Kitoko City in the Democratic Republic of Congo—a new city project officially launched in 2019 but never implemented—this article examines the political, social, and spatial effects generated by urban initiatives that remain at the stage of intention. It investigates how such unbuilt projects
Patrick Belinga Ondoua
wiley   +1 more source

Investigation of internal ballistics of solid propellant rocket motor by numerical and experimental methods. [PDF]

open access: yes, 2020
The dissertation discusses the relevant case of the development of a unified construction methodology for solid-propellant rocket motors, based on numerical modelling of internal ballistics of the motor, evaluating the energy properties of the solid ...
Račkauskas, Saulius,
core   +1 more source

Past and Present Large Solid Rocket Motor Test Capabilities [PDF]

open access: yes, 2011
A study was performed to identify the current and historical trends in the capability of solid rocket motor testing in the United States. The study focused on test positions capable of testing solid rocket motors of at least 10,000 lbf thrust.
Owen, David B., II, Kowalski, Robert R.
core  

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