Multidisciplinary design optimization of a wide speed range vehicle with waveride airframe and RBCC engine

T Zhang, X Yan, W Huang, X Che, Z Wang - Energy, 2021 - Elsevier
The wide speed range vehicle is believed to be ideal for space round trip and its design
process incorporates a number of disciplines. To achieve an overall optimal design, we …

CMDOWS: a proposed new standard to store and exchange MDO systems

I van Gent, G La Rocca, MFM Hoogreef - CEAS Aeronautical Journal, 2018 - Springer
This paper proposes a new format to store and exchange multidisciplinary design
optimization (MDO) systems. Here, the generic term MDO system refers to the set of …

All-At-Once formulation integrating pseudo-spectral optimal control for launch vehicle design and uncertainty quantification

M Balesdent, L Brevault, JL Valderrama-Zapata… - Acta Astronautica, 2022 - Elsevier
Launch vehicle design is a multidisciplinary process involving different disciplines such as
aerodynamics, structure, propulsion and trajectory. This latter is a key discipline in the …

Multidisciplinary design optimization and analysis of hydrazine monopropellant propulsion system

A Adami, M Mortazavi, M Nosratollahi… - International Journal …, 2015 - Wiley Online Library
Monopropellant propulsion systems are widely used especially for low cost attitude control
or orbit correction (orbit maintenance). To optimize the total propulsion system, subsystems …

[HTML][HTML] Multidisciplinary design optimization of a dual-spin guided vehicle

J Karimi, MR Rajabi, SH Sadati, SM Hosseini - Defence Technology, 2024 - Elsevier
In this research, a Multidisciplinary Design Optimization approach is proposed for the dual-
spin guided flying projectile design considering external and internal parts of the body as …

Performance comparison between waverider and wide-speed-range gliding vehicle based on CFD approaches

TT Zhang, ZG Wang, W Huang, XT Yan - Science China Technological …, 2019 - Springer
Wide-speed-range gliding vehicle (WSRGV) is designed to adapt to the variable cruising
environment that hypersonic vehicles will encounter during the mission implementation …

Multi-disciplinary system design optimization of a launch vehicle upper-stage

M Zakeri, M Nosratollahi, A Novinzade - Journal of Aerospace …, 2017 - SciELO Brasil
The design method presented in this paper is related to the upper-stage system and its
instrumentation, expedition and facilitation so as to transfer the satellite from the destination …

Optimization of 10 N Monopropellant High Test Peroxide Thruster for Space Applications

F Benzenine, C Seladji, D Darfilal… - Journal of Advanced …, 2022 - semarakilmu.com.my
Monopropellant thruster is one of the most propulsion system types developed in the space
industry. This system uses a single type of propellant that reacts in porous medium catalytic …

Design of an Upper Stage Propulsion System by Multi Objective Hybrid PSO

M Nosratollahi, MF Fatehi, A Adami - Journal of Space Science and …, 2020 - jsstpub.com
Orbital transfer blocks has the task of transferring satellites to objective orbits from parking
orbit. In this paper, Attention will be given to multidisciplinary optimal design of the …

Optimization of potassium nitrate based solid propellant grains formulation using response surface methodology

OO Ogunleye, JO Hammed, SO Alagbe - Advances in Science and …, 2015 - infona.pl
This study was designed to evaluate the effect of propellant formulation and geometry on the
solid propellant grains internal ballistic performance using core, bates, rod and tubular and …