Space systems design (spacecraft, satellites, space stations and their equipment)
Performance evaluation of a launch vehicle with non-turbopump propulsion system based on multidisciplinary analysis (MDA)

Hanieh Eshaghnia; Mehran Nosratollahi; Amirhossain Adami

Volume 14, Issue 4 , December 2021, , Pages 35-49

Abstract
  A new approach to the design and development of launchers is the use of advanced technologies to reduce design and development costs as much as possible. In this paper, an approach to reduce costs and increase reliability is proposed, which is based on the use of a non-turbo pump propulsion system (pressure-fed ...  Read More

Space Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach

Hasan Naseh

Volume 9, Issue 4 , April 2017, , Pages 1-12

Abstract
  The major purpose of this paper is to present Space Launch System (SLS) family technology development from propulsion system aspect. Thus, the models of cost estimation for two types of propulsion systems (cryogenic and semi-cryogenic) are derived based on the statistical method and are then compared ...  Read More