**Author details**

Ozan Kara1,2\*† and Arif Karabeyoglu<sup>2</sup>

1 DeltaV Space Technologies Inc., Istanbul, Turkey

2 Department of Mechanical Engineering, KOC University, Istanbul, Turkey

\*Address all correspondence to: okara13@ku.edu.tr

† These authors contributed equally.

© 2021 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/ by/3.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

*Hybrid Propulsion System: Novel Propellant Design for Mars Ascent Vehicles DOI: http://dx.doi.org/10.5772/intechopen.96686*
