publication . Conference object . 2017

Multi-objective optimisation for spacecraft design for demise and survivability

Mirko Trisolini;
Open Access English
  • Published: 01 Nov 2017
  • Country: United States
The paper presents the development of a multi-objective optimisation framework to study the effects that preliminary design choices have on the demisability and the survivability of a spacecraft. Building a spacecraft such that most of it will demise during the re-entry through design-for-demise strategies may lead to design that are more vulnerable to space debris impacts, thus compromising the reliability of the mission. The two models developed to analyse the demisability and the survivability are presented and used as the objective functions of the multi-objective optimisation of the external structure of a simplified spacecraft configuration. The results ar...
arXiv: Physics::Space PhysicsPhysics::History of PhysicsAstrophysics::Earth and Planetary Astrophysics
Related Organizations
Download fromView all 2 versions
e-Prints Soton
Conference object . 2017
Powered by OpenAIRE Research Graph
Any information missing or wrong?Report an Issue