Low-Cost Satellite Launch System—Aerodynamic Feasibility Study.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Jun2022, Vol. 9 Issue 6, pN.PAG-N.PAG, 21p
- Subject
FINITE volume method SPACE vehicles ARTIFICIAL satellite launching PARTIAL differential equations MICROSPACECRAFT WIND tunnels AIRCRAFT carriers - Language
- ISSN
- 22264310