Development of 200 N-class throttleable hybrid rocket motor for lunar module application
In this study, ground tests of a lab-scale hybrid rocket motor were conducted to verify the feasibility of the hybrid propulsion system for lunar lander application. The primary goal is to assess the realizability of hybrid rocket by testing its throttleability and soft landing capability with a sca...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
KeAi Communications Co. Ltd.
2021-12-01
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| Series: | FirePhysChem |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2667134421000602 |