Mathematical Model and Performance Evaluation for a Small Orbital Launcher-Reference-Cited by-同舟云学术

Mathematical Model and Performance Evaluation for a Small Orbital Launcher

Published:2015-07 Issue: Volume:772 Page:388-394
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Chelaru Teodor Viorel¹,Chelaru Adrian²

Affiliation:

1. University POLITEHNICA of Bucharest

2. INCAS -National Institute for Aerospace Research “Elie Carafoli

Abstract

The purpose of this paper is to present some aspects regarding the computational model and simulation for three stage launch vehicle (LV) used to inject in orbit small size payload. The computational model consists in numerical simulation of LV evolution for imposed start conditions. The launcher model presented will be with six degrees of freedom (6DOF) and variable mass. The results analysed will be the flight parameters and ballistic performances. The discussions area will focus around the technical possibility to realize a small multi-stage launcher, end evaluate his performance using the developed model. From technical point of view, the paper is focused on ESA project “Study – concept, to achieve a Small Orbital Launcher through zonal cooperation - SOL

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.772.388.pdf

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