Journals
Publish with us
Publishing partnerships
About us
Blog
International Journal of Aerospace Engineering
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
International Journal of Aerospace Engineering
/
2021
/
Article
/
Fig 13
/
Research Article
Design Optimization and Parameter Analysis of a Hybrid Rocket Motor-Powered Small LEO Launch Vehicle
Figure 13
Height-time curve of different cases: (a) whole flight; (b) glide phase and 3rd-stage working phase.
(a)
(b)