Design and Feasibility Study of Novel Flying Wing Carrier for Launching Small Satellites in Low Earth Orbit

Autor: Mario R. Chiarelli, Fabiano B. Borrometi, Vittorio Cipolla, Vincenzo Binante, Karim Abu Salem, Giuseppe Palaia

Publikováno v: Applied Sciences, Vol 13, Iss 8, p 4712 (2023)

In recent years, there has been a considerable growth in the demand for low-orbit satellites, leading to a need for more flexible and cost-effective launch systems. This study presents a low-cost “carrier-launcher” configuration designed for spac

Externí odkaz: https://doaj.org/article/07e420dadf2e40c5a0b123d8ad68b635

Low-Cost Satellite Launch System—Aerodynamic Feasibility Study

Autor: Dziubiński, Aleksander Olejnik, Łukasz Kiszkowiak, Piotr Zalewski, Adam

Publikováno v: Aerospace; Volume 9; Issue 6; Pages: 284

In recent decades, the rapid development of alternative methods for launching satellites into space has been observed. The main purpose of this work is to obtain reliable information about aerodynamic properties, which will be useful in the prelimina

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=multidiscipl::12e115451ea9c378fe3ba4db8ea81810

Rocket Design and Structural Modeling & Analysis of Micro-Satellite Launch Vehicle: Inspired by VECTOR-R

Autor: NOSSEIR, AHMED E. S.

Micro-satellite launch vehicles are currently being developed in a rapid manner to fulfill needs of Micro- and Nano- satellites market, mainly for scientific and research uses. Light-weight structures and composite materials are key aspects in develo

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::73e4ef2dccd8706381cfd5fa7e9620ff

Three dimensional supersonic flow analysis over a satellite vehicle launcher

Autor: A. L. De Bortoli

Publikováno v: Journal of Computational and Applied Mathematics. 103:33-41

The ever-widening applications of numerical calculations leads to a variety of new numerical methods, which are different in their solution algorithms as well as in the discretization of the governing equations. Despite this development, much work st

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6d7a4d56cbf690b1e5de8ada61e13a3e
https://doi.org/10.1016/s0377-0427(98)00238-6

Three-dimensional viscous flow simulations over the VLS using overset grids

Autor: J. L. F. Azevedo, E. Basso

Publikováno v: Journal of the Brazilian Society of Mechanical Sciences and Engineering v.26 n.4 2004
Journal of the Brazilian Society of Mechanical Sciences and Engineering
Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron:ABCM
Journal of the Brazilian Society of Mechanical Sciences and Engineering, Volume: 26, Issue: 4, Pages: 438-445, Published: DEC 2004

The present work is inserted into an effort to develop a Chimera flow simulation code capable of handling general launch vehicle configurations. The paper is primarily concerned with presenting results of laminar and turbulent viscous simulations of

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c1fd032297579b35a0701de8efb61da9
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1678-58782004000400009