Effects of geometrical parameters of a two-sided catalyst bed on flow and thermal fields of a monopropellant hydrazine thruster
MR Salimi - Journal of Space Science and Technology, 2022 - jsstpub.com
In present study, a hydrazine based monopropellant thruster decomposition chamber is
simulated numerically. The catalyst bed separated in two sides, the particles size in …
simulated numerically. The catalyst bed separated in two sides, the particles size in …
[PDF][PDF] Design and Configuration of Ground Sample Components of Low Propulsion Monopropellant Thruster Using Some Engineering Software
S Davari, H Karimaei, MR Salimi… - Journal of Space …, 2021 - pdfs.semanticscholar.org
Monopropellant thruster are used to inject a satellite into orbit or control its position on three
axes in space missions. One of them is hydrazine thruster which is widely used. In this …
axes in space missions. One of them is hydrazine thruster which is widely used. In this …
Metamodeling by kriging method for the disciplines of liquid hydrazine monopropellant propulsion system using Latin hypercube sampling method
MH Mansouri Moghari, H Naseh, S Nouri - Aerospace Knowledge and …, 2023 - astjournal.ir
When designing complex products such as space thrusters, accurate simulation models are
needed to evaluate and improve the design during development. The implementation of …
needed to evaluate and improve the design during development. The implementation of …
تولید فرامدل به روش کرایگینگ برای موضوعات سامانه رانشگر تک پیشرانه مایع هیدرازینی با استفاده از روش نمونه برداری ابرمکعب لاتین
منصوری موغاری, ناصح, حسن, نوری - دانش و فناوری هوافضا, 2023 - astjournal.ir
در فرآیند طراحی محصولات پیچیده مانند رانشگرهای فضایی، برای ارزیابی و بهبود طرح، مدلها و
شبیهسازیهای دقیق مورد نیاز هستند. دستیابی به این مدلهای دقیق، اغلب پر هزینه و زمانبر …
شبیهسازیهای دقیق مورد نیاز هستند. دستیابی به این مدلهای دقیق، اغلب پر هزینه و زمانبر …