Analysis of Propellant Weight under Re-Entry Conditions for a Reusable Launch Vehicle Using Retropropulsion
In this study, a minimum amount of required propellant was calculated by analyzing the sequence with various re-entry conditions. This study aims to obtain data related to variation in trajectory and required propellant weight according to various re-entry scenarios. The drag coefficient at various...
שמור ב:
| Principais autores: | , , |
|---|---|
| פורמט: | Artigo |
| שפה: | Inglês |
| יצא לאור: |
MDPI AG
2021-05-01
|
| סדרה: | Energies |
| נושאים: | |
| גישה מקוונת: | https://www.mdpi.com/1996-1073/14/11/3210 |
| תגים: |
אין תגיות, היה/י הראשונ/ה לתייג את הרשומה!
|